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USA National Advisory Committee for Aeronautics

Technical notes / National Advisory Committee for Aeronautics

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Medientyp: Schriftenreihe; Monographische Schriftenreihe
Titel: Technical notes / National Advisory Committee for Aeronautics
Weitere Titel: Nebent.: Technical note
Nebent.: NACA technical notes
Beteiligte: USA National Advisory Committee for Aeronautics
Erschienen: Washington, DC, 1920-1958
Erscheinungsverlauf: Nr. 1.1920 - 4410.1958
Sprache: Nicht zu entscheiden
ISSN: 0097-2177
Schlagwörter: Monografische Reihe
Entstehung:
Anmerkungen:

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Gault, Donald E. [VerfasserIn]
3963: A correlation of low-speed, airfoil-section stalling characteristics with Reynolds number and airfoil geometry by Donald E. Gault
Washington, DC: National Advisory Committee for Aeronautics, 1957

Williams, James L. [VerfasserIn]
3645: Wind-tunnel investigation of effects of fuselage cross sectional shape, fuselage bend, and vertical tail size on directional characterstics of nonoverlap-type helicopter fuselage models without rotors by James L. Williams
Washington, DC: National Advisory Committee for Aeronautics, 1956

Loftin, Laurence K. [VerfasserIn]
3241: Airfoil section characteristics at high angles of attack by Laurence K. Loftin
Washington, DC: National Advisory Committee for Aeronautics, 1954

Queijo, M. J. [VerfasserIn]; Riley, Donald R. [VerfasserIn]
3245: Calculated subsonic span loads and resulting stability derivatives of unswept and 45° sweptback tail surfaces in sideslip and in steady roll by M. J. Queijo and Donald R. Riley
Washington, DC: National Advisory Committee for Aeronautics, 1954

Levin, L. Ross [VerfasserIn]
2930: Strength analysis of stiffened thick beam webs with ratios of web depth to web thickness of approximately 60 by L. Ross Levin
Washington, DC: National Advisory Committee for Aeronautics, 1953

Van Dyke, Milton [VerfasserIn]
2670: High-speed subsonic characteristics of 16 NACA 6-series airfoil sections by Milton D. Van Dyke
Washington, DC: National Advisory Committee for Aeronautics, 1952

Hubbard, Harvey H. [VerfasserIn]
2701: A Survey of the aircraft-noise problem with special reference to its physical aspects by Harvey H. Hubbard
Washington, DC: National Advisory Committee for Aeronautics, 1952

Elwell, Fred S. [VerfasserIn]
2728: Experiments to determine neighborhood reactions to light airplanes with and without external noise reduction by Fred S. Elwell
Washington, DC: National Advisory Committee for Aeronautics, 1952

Kuhn, Paul [VerfasserIn]; Peterson, James P. [VerfasserIn]; Levin, L. Ross [VerfasserIn]
2661: A summary of diagonal tension 1 Methods of analysis by Paul Kuhn; James P. Peterson and L. Ross Levin
Washington: NACA, 1952

Racisz, Stanley F. [VerfasserIn]
2824: Effects of independent variations of mach number and Reynolds number of the maximum lift coefficients of four NACA 6-series airfoil sections by Stanley F. Racisz
Washington, DC: National Advisory Committee for Aeronautics, 1952

Flügge, Wilhelm [VerfasserIn]
2743: Landing-gear impact by W. Flügge
Washington, DC: National Advisory Committee for Aeronautics, 1952

Kraft, Christopher C. [VerfasserIn]; Assadourian, Arthur [VerfasserIn]
2415: Experimental study of an angle-of-attack vane mounted ahead of the nose of an airplane for use as a sensing device for an acceleration alleviator by Christopher C. Kraft and Arthur Assadourian
Washington, DC: National Advisory Committee for Aeronautics, 1951

Brewer, Jack D. [VerfasserIn]; Fisher, Lewis R. [VerfasserIn]
2555: Effect of taper ratio on the low-speed rolling stability derivatives of swept and unswept wings of aspect ratio 2.61 by Jack D. Brewer and Lewis R. Fisher
Washington, DC: National Advisory Committee for Aeronautics, 1951

McCullough, George B. [VerfasserIn]; Gault, Donald E. [VerfasserIn]
2502: Examples of three representative types of airfoil-section stall at low speed by George B. McCullough and Donald E. Gault
Washington: National Advisory Committee for Aeronautics, 1951

Taylor, Marion K. [VerfasserIn]
2220: A balsa-dust technique for air-flow visualization and its application to flow through model helicopter rotors in static thrust by Marion K. Taylor
Washington, DC: National Advisory Committee for Aeronautics, 1950

Loftin, Laurence K. [VerfasserIn]; Smith, Hamilton A. [VerfasserIn]
1945: Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 + 10 6 to 9.0. x 10 6 by Laurence K. Loftin and Hamilton A. Smith
Washington: NACA, 1949

Ward, Kenneth E. [VerfasserIn]
749: A new method of studying the flow of the water along the bottom of a model of a flying boat hull by Kenneth E. Ward
[Washington, DC]: NACA, [1940]

London, Albert [VerfasserIn]
748: Principles, practice, and progress of noise reduction in airplanes by Albert London
Washington, DC: NACA, 1940

Rodert, Lewis A. [VerfasserIn]
712: A preliminary study of the prevention of ice on aircraft by the use of engine exhaust by Lewis A. Rodert
[Washington, D.C.]: NACA, 1939

Harris, Thomas A. [VerfasserIn]
715: Wind tunnel investigation of an NACA 23012 airfoil with two arrangements of a wide-chord slotted flap by Thomas A. Harris
[Washington, DC]: NACA, [1939]

Wetmore, J. W. [VerfasserIn]
714: Flight tests of retractable ailerons on a highly tapered wing by J. W. Wetmore
[Washington, DC]: NACA, [1939]

Dunn, Louis G. [VerfasserIn]
752: An investigation of sheet stiffener panels subjected to compression loads with particular reference to torsionally weak stiffeners by Louis G. Dunn
[Washington, DC]: NACA, [1939?]

Duschinsky, Frank [VerfasserIn]
728: Wind tunnel investigation of an NACA 23021 airfoil with two arrangements of a 40 percent chord slotted flap by Frank Duschi[nsky]
[Washington, DC]: NACA, [1939]

Donely, Philip [VerfasserIn]; Shufflebarger, C. C. [VerfasserIn]
731: Tests in the gust tunnel of a model of the XBM-1 airplane by Philip Donely and C. C. Shufflebarger
Washington, D.C.: NACA, 1939

Weiss, Herbert K. [VerfasserIn]
700: Theory of automatic control of airplanes by Herbert K. Weiss
Washington, DC: NACA, 1939

Bamber, Millard J. [VerfasserIn]; House, Rufus O. [VerfasserIn]
703: Wind tunnel investigation of effect of yaw on lateral stability characteristics 1 Four NACA 23012 wings of various plan forms with and without dihedral by M. J. Bamber and R. O. House
[Washington, DC]: NACA, 1939

Hood, Manley J. [VerfasserIn]
724: The effects of surface waviness and of rib stitching on wing drag by Manley J. Hood
[Washington, DC]: NACA, [1939]

Hood, Manley J. [VerfasserIn]
695: The effects of some common surface irregula[rities] on wing drag by Manley J. Hood
[Washington, DC]: NACA, [1939]

Recant, Isidore G. [VerfasserIn]
705: Wind tunnel investigation of ground effect on wings with flaps by Isidore G. Recant
Washington, D.C.: NACA, 1939

Anderson, Raymond F. [VerfasserIn]
713: A comparison of several tapered wings designed to avoid tip stalling by Raymond F. Anderson
[Washington, DC]: NACA, [1939]

Ramberg, Walter [VerfasserIn]; MacPherson, Albert E. [VerfasserIn]; Levy, Sam [VerfasserIn]
721: Compressive tests of a monocoque box by Walter Ramberg, Albert E. McPherson, and Sam Levy
[Washington, DC]: NACA, [1939]

Street, William G. [VerfasserIn]; Ames, Milton B. [VerfasserIn]
734: Pressure distribution investigation of an NACA 0009 airfoil with a 50 percent chord plain flap and three tabs by William G. Street and Milton B. Ames, jr
[Washington, DC]: NACA, [1939]

Bamber, Millard J. [VerfasserIn]; House, Rufus O. [VerfasserIn]
730: Wind tunnel investigation of effect of yaw on lateral stability characteristics 2 Rectangular NACA 23012 wing with a circular fuselage and a fin by M. J. Bamber and R. O. House
[Washington, DC]: NACA, 1939

Weller, R. [VerfasserIn]; Bussey, J. K. [VerfasserIn]
737: Photoelastic analysis of three-dimensional stress systems using scattered light by R. Weller and J. K. Bussey
[Washington, DC]: NACA, [1939]

Troller, Theodor [VerfasserIn]; Rokus, Frank [VerfasserIn]
735: Pressure distribution measurements on a tapered wing with a partial span split flap in curved flight by Th. Troller and F. Rokus
Washington, DC: NACA, 1939

Rokus, Frank [VerfasserIn]
742: Pressure distribution measurements on a [rectangular wing] with a partial span split flap in [curved flight] by Frank G. Rokus
[Washington, DC]: NACA, 1939

Parkinson, John B. [VerfasserIn]; Olson, Roland E. [VerfasserIn]; House, Rufus O. [VerfasserIn]
716: Hydrodynamic and aerodynamic tests of a family of models of seaplane floats with varying angles of dead rise NACA models 57-A, 57-B, and 57-C by John B. Parkinson, Roland E. Olson, and R. O. House
Washington: NACA, 1939

Sherman, Albert [VerfasserIn]
732: A simple method of obtaining span load distributions by Albert Sherman
Washington, D.C.: NACA, 1939

Wildhack, W. A. [VerfasserIn]; Goerke, V. H. [VerfasserIn]
738: Corrugated metal diaphragms for aircraft pressure measuring instruments by W. A. Wildhack and V. H. Goerke
Washington, D.C.: NACA, 1939

House, Rufus O. [VerfasserIn]
719: The effects of partial span slotted flaps on the aerodynamic characteristics of a rectangular and a tapered NACA 23012 [airfoil] by Rufus O. House
[Washington]: NACA, [1939]

Seidman, Oscar [VerfasserIn]; Donlan, Charles J. [VerfasserIn]
711: An approximate spin design criterion for monoplanes by Oscar Seidman and Charles J. Donlan
[Washington, DC]: NACA, [1939]

Donely, Philip [VerfasserIn]; Shufflebarger, C. C. [VerfasserIn]
745: Tests of a gust alleviating flap in [...] by Philip Donely and C. C. Shufflebarger
Washington, D.C.: NACA, 1939

Lundquist, Eugene E. [VerfasserIn]
717: A method of estimating the critical buckling load for structural members by Eugene E. Lundquist
[Washington, DC]: NACA, [1939]

Lundquist, Eugene E. [VerfasserIn]
722: Local instability of centrality loaded columns of channel section and Z-section by Eugene E. Lundquist
[Washington, DC]: NACA, [1939]

Rothrock, A. M. [VerfasserIn]; Selden, Robert F. [VerfasserIn]
723: Adhesion of ice in its relation to the de-icing of airplanes by A. M. Rothrock and R. F. Selden
[Washington, DC]: NACA, [1939]

Gottlieb, R. [VerfasserIn]; Thompson, T. M. [VerfasserIn]; Witt, E. C. [VerfasserIn]
726: Combined beam column stresses of aluminium alloy channel sections by R. Gottlieb, T. M. Thompson and E. C. Witt
[Washington, DC]: NACA, [1939]

Dumont, C. [VerfasserIn]
740: Stress concentration around an open circular hole in a plate subjected to bending [normal] to the plane of the [plate] by C. Dumont
[Washington, DC]: NACA, 1939

Bailey, F. J. [VerfasserIn]; Gustafson, F. B. [VerfasserIn]
741: Observations in flight of the region of stalled flow over the blades of an autogiro rotor by F. J. Bailey, jr., and F. B. Gustafson
Washington, DC: NACA, 1939

Diehl, Walter S. [VerfasserIn]
692: Some fundamental considerations in regard to the use of power in landing an airplane by Walter S. Diehl
[Washington, DC]: NACA, [1939]

House, Rufus O. [VerfasserIn]
680: The aerodynamic drag of five models of side floats NACA models 51-E, 51-F, 51-G, 51-H, and 51-J by R. O. House
[Washington]: NACA, [1938]

Seidman, Oscar [VerfasserIn]; Neihouse, Anshal I. [VerfasserIn]
664: Free spinning wind tunnel tests of a low wing monoplane with systematic changes in wings and tails 3 Mass distributed along the wings by Oscar Seidman and A. I. Neihouse
[Washington, DC]: NACA, 1938

Kuethe, Arnold M. [VerfasserIn]
685: Circulation measurements about the tip of an airfoil during flight through a gust by Arnold M. Kuethe
[Washington, DC]: NACA, [1938]

Jones, Robert T. [VerfasserIn]
682: The unsteady lift of a finite wing by Robert T. Jones
[Washington, DC]: NACA, [1938]

Lundquist, Eugene E. [VerfasserIn]
658: Generalized analysis of experimental observations in problems of elastic stability by Eugene E. Lundquist
[Washington, DC]: NACA, [1938]

Lundquist, Eugene E. [VerfasserIn]; Kroll, W. D. [VerfasserIn]
652: Tables of stiffness and carry over factor for structural members under axial load by Eugene E. Lundquist and W. D. Kroll
[Washington, DC]: NACA, [1938]

Stack, John [VerfasserIn]; Lindsey, W. F. [VerfasserIn]
665: Tests of N-85, N-86, and N-87 airfoil sections in the 11-inch high-speed wind tunnel by John Stack and W. F. Lindsey
[Washington, DC]: NACA, [1938]

Benson, William M. [VerfasserIn]
677: Tests of a contra-propeller for aircraft by William M. Benson
Washington, DC: NACA, 1938

Bamber, Millard J. [VerfasserIn]
702: Wind tunnel tests of several forms of fixed wing slot in combination with a slotted flap on an N.A.C.A. 23012 airfoil by M. J. Bamber
[Washington, D.C.]: NACA, [1938]

Sherman, Albert [VerfasserIn]
642: Interference of wing and fuselage from tests of eight combinations in the NACA variable density tunnel combinations with tapered fillets and straight side junctures by Albert Sherman
[Washington]: NACA, [1938]

Brevoort, Maurice J. [VerfasserIn]
649: The effect of air passage length on the optimum fin spacing for maximum cooling by Maurice J. Brevoort
Washington, DC: NACA, 1938

Klemin, Alexander [VerfasserIn]; Pepper, Perry A. [VerfasserIn]; Wittner, Howard A. [VerfasserIn]
666: Longitudinal stability in relation to the use of an automatic pilot by Alexander Klemin, Perry A. Pepper, and Howard A. Wittner
[Washington, DC]: NACA, [1938]

Hartman, Edwin P. [VerfasserIn]
646: Wind tunnel tests of a 2-engine airplane model as a preliminary study of flight conditions arising on the failure of one engine by Edwin P. Hartman
[Washington, DC]: NACA, [1938]

Wenzinger, Carl J. [VerfasserIn]; Rogallo, Francis M. [VerfasserIn]
690: Résumé of air load data on slats and flaps by Carl J. Wenzinger and Francis M. Rogallo
[Washington, DC]: NACA, [1938]

Diehl, Walter S. [VerfasserIn]
643: A study of flying boat take-off by Walter S. Diehl
[Washington, DC]: NACA, [1938]

Bleakney, William M. [VerfasserIn]
660: Fatigue testing of wing beams by the resonance method by William M. Bleakney
[Washington, DC]: NACA, [1938]

Doenhoff, Albert E. von [VerfasserIn]
671: A method of rapidly estimating the position of the laminar separation point by Albert E. von Doenhoff
[Washington, DC]: NACA, [1938]

Parkinson, John B. [VerfasserIn]; House, Rufus O. [VerfasserIn]
656: Hydrodynamic and aerodynamic tests of models of floats for single float seaplanes NACA models 41-D, 41-E, 61-A, 73, [and 73-A] by J. B. Parkinson and R. O. House
[Washington]: NACA, [1938]

Jones, Robert T. [VerfasserIn]
667: Operational treatment of the nonuniform-lift theory in airplane dynamics by Robert T. Jones
Washington, DC: NACA, 1938

Stickle, George W. [VerfasserIn]; Joyner, Upshur T. [VerfasserIn]
673: The pressure available for ground cooling in front of the cowling of air cooled airplane engines by George W. Stickle and Upshur T. Joyner
Washington, DC: NACA, 1938

Soulé, Hartley A. [VerfasserIn]; Hootman, James A. [VerfasserIn]
653: A flight investigation of the reduction of aileron operating force by means of fixed tabs and differential linkage, with notes on linkage design by Hartley A. Soulé and James A. Hootman
[Washington, DC]: NACA, [1938]

Wenzinger, Carl J. [VerfasserIn]; Ames, Milton B. [VerfasserIn]
661: Wind tunnel investigation of rectangular and tapered NACA 23012 wings with plain ailerons and full span split flaps by Carl J. Wenzinger and Milton B. Ames
[Washington, DC]: NACA, [1938]

House, Rufus O. [VerfasserIn]
663: The effects of partial span plain flaps on the aerodynamic characteristics of a rectangular and a tapered Clark Y [wing] by R. O. House
[Washington]: NACA, [1938]

Sherman, Albert [VerfasserIn]
641: Interference of wing and fuselage from tests of 17 combinations in the NACA variable density tunnel combinations with special junctures by Albert Sherman
[Washington]: NACA, [1938]

Abbott, Ira H. [VerfasserIn]; Sherman, Albert [VerfasserIn]
672: Flow observations with tufts and lampblack of the stalling of four typical airfoil sections in the NACA variable density tunnel by Ira H. Abbott and Albert Sherman
[Washington]: NACA, [1938]

Fishbein, Meyer [VerfasserIn]
694: Physical properties of synthetic res[ins] by Meyer Fishbein
[Washington, DC]: NACA, [1938]

Moore, R. L. [VerfasserIn]; Paul, D. A. [VerfasserIn]
696: Torsional stability of aluminium alloy seamless tubing by R. L. Moore and D. A. Paul
[Washington, DC]: NACA, [1938]

Sherman, Albert [VerfasserIn]
640: Interference of wing and fuselage from tests of 18 combinations in the NACA variable density tunnel combinations with split flaps by Albert Sherman
[Washington]: NACA, [1938]

Imlay, Frederick H. [VerfasserIn]
636: The estimation of the rate of change of yawing moment with sideslip by Frederick H. Imlay
[Washington, DC]: NACA, [1938]

Doenhoff, Albert E. von [VerfasserIn]
639: A preliminary investigation of boundary layer transition along a flat plate with adverse pressure gradient by Albert E. von Doenhoff
[Washington, DC]: NACA, [1938]

Soulé, Hartley A. [VerfasserIn]; Gough, Melvin N. [VerfasserIn]
645: Some aspects of the stalling of modern low wing monoplanes by Hartley A. Soulé and Melvin N. Gough
[Washington, DC]: NACA, [1938]

Wenzinger, Carl J. [VerfasserIn]; Bamber, Millard J. [VerfasserIn]
659: Wind tunnel tests of three lateral control devices in combination with a full span slotted flap on an NACA 23012 airfoil by Carl J. Wenzinger and Millard J. Bamber
[Washington, DC]: NACA, [1938]

Bamber, Millard J. [Sonstige Person, Familie und Körperschaft]; House, Rufus O. [Sonstige Person, Familie und Körperschaft]
625: Spinning characteristics of wings 4 Changes in stagger of rectangular Clark Y biplane cellules / by M. J. Bamber and R. O. House by M. J. Bamber and C. H. Zimmerman
[Washington, DC]: NACA, 1937

Gauvain, William E. [VerfasserIn]
598: Wind tunnel tests of a Clark Y wing with "Maxwell" leading edge slots by William E. Gauvain
[Washington, DC]: NACA, [1937]

Dätwyler, G. [VerfasserIn]
520: Calculations of the effect of wing twist on the air forces acting on a monoplane wing by G. Dätwyler
[Washington, DC]: NACA, [1937?]

Soulé, Hartley A. [VerfasserIn]; Gracey, William [VerfasserIn]
632: Improvement of aileron effectiveness by the prevention of air leakage through the hinge gap as determined in flight by Hartley A. Soulé and W. Gracey
[Washington, DC]: NACA, [1937]

Kline, G. M. [VerfasserIn]
628: Plastics as structural materials [...] by G. M. Kline
[Washington, DC]: NACA, [1937]

Soulé, Hartley A. [VerfasserIn]
597: Notes on the calculation of the minimum horizontal tail surface for airplanes equipped with wing flaps by Hartley A. Soulé
[Washington, DC]: NACA, [1937]

Sontag, Harcourt [VerfasserIn]; Johnson, Daniel P. [VerfasserIn]
624: Performance characteristics of venturi tubes used in aircraft for operating air driven gyroscopic instruments by Harcourt Sontag and Daniel P. Johnson
[Washington, DC]: NACA, [1937]

Clauser, Milton [VerfasserIn]; Clauser, Francis [VerfasserIn]
613: The effect of curvature on the transition from laminar to turbulent boundary layer by Milton Clauser and Francis Clauser
Washington, D.C.: NACA, 1937

Bamber, Millard J. [Sonstige Person, Familie und Körperschaft]; House, Rufus O. [Sonstige Person, Familie und Körperschaft]
633: Spinning characteristics of wings 5 NACA 0009, 23018, and 6718 mono[planes] / by M. J. Bamber and R. O. House by M. J. Bamber and C. H. Zimmerman
[Washington, DC]: NACA, 1937

Seidman, Oscar [VerfasserIn]; Neihouse, Anshal I. [VerfasserIn]
620: Free spinning wind tunnel tests of a low wing monoplane with systematic changes in wings and tails 2 Mass distributed along the fuselage by Oscar Seidman and A. I. Neihouse
[Washington, DC]: NACA, 1937

Lesley, E. P. [VerfasserIn]
689: Tandem air propellers by E. P. Lesley
[Washington, D.C.]: NACA, [1937]

Abbott, Ira H. [VerfasserIn]
614: Fuselage drag tests in the variable density wind tunnel streamline bodies of revolution, fineness ratio of 5 by Ira H. Abbott
[Washington]: NACA, [1937]

Lundquist, Eugene E. [VerfasserIn]
617: Stability of structural members under axial load by Eugene E. Lundquist
[Washington, DC]: NACA, [1937]

Niles, Alfred S. [VerfasserIn]; Buckwalter, John C. [VerfasserIn]; Reed, Warren D. [VerfasserIn]
595: Bending tests of circular cylinders of corrugated aluminium alloy sheet by Alfred S. Niles, John C. Buckwalter, and Warren D. Reed
[Washington]: NACA, [1937]

MacAvoy, William H. [VerfasserIn]
623: Maximum forces applied by pilots to wheel type controls by William H. McAvoy
[Washington, DC]: NACA, [1937]

Wenzinger, Carl J. [VerfasserIn]
650: Wind tunnel tests of a Clark Y wing having split flaps with gaps by Carl J. Wenzinger
[Washington, DC]: NACA, [1937]

Pearson, Henry A. [VerfasserIn]
589: Theoretical span loading and moments of tapered wings produced by aileron deflection by H. A. Pearson
Washington, D.C.: NACA, 1937

Parsons, John F. [VerfasserIn]; Silverstein, Abe [VerfasserIn]
591: Full scale span load distribution on a tapered wing with SPLIT flaps of various spans by John F. Parsons and Abe Silverstein
Washington, D.C.: NACA, 1937

Thompson, F. L. [VerfasserIn]
616: The measurement of air speed of airplanes by F. L. Thompson
[Washington, DC]: NACA, [1937]

Dearborn, Clinton H. [VerfasserIn]; Soulé, Hartley A. [VerfasserIn]
596: Full scale wind tunnel and flight tests of a Fairchild 22 airplane equipped with a Zap flap and Zap ailerons by C. H. Dearborn and H. A. Soulé
[Washington, DC]: NACA, [1937]

Soulé, Hartley A. [VerfasserIn]; Hootman, James A. [VerfasserIn]
622: Flight tests of an airplane showing dependence of the maximum lift coefficient on the test conditions by H. A. Soulé and James A. Hootman
[Washington, DC]: NACA, [1937]

Wenzinger, Carl J. [VerfasserIn]
627: Pressure distribution over a Clark Y-H airfoil section with a split flap by Carl J. Wenzinger
[Washington, DC]: NACA, [1937]

Hartman, Edwin P. [VerfasserIn]
557: Considerations of the take-off problem by Edwin P. Hartman
[Washington, DC]: NACA, [1936]

Gough, Melvin N. [VerfasserIn]
553: Notes on the technique of landing airplanes equipped with wing flaps by Melvin N. Gough
[Washington, DC]: NACA, [1936]

Parsons, John F. [VerfasserIn]
561: Full scale wind tunnel tests to determine a satisfactory location for a service pitot static tube on a low wing monoplane by John F. Parsons
Washington, D.C.: NACA, 1936

Jones, Robert T. [VerfasserIn]; Nerken, Albert I. [VerfasserIn]
586: The reduction of aileron operating force by differential linkage by Robert T. Jones and Albert I. Nerken
Washington, D.C.: NACA, 1936

Bell, Joe W. [VerfasserIn]
566: Tank tests of a model of the NC flying boat hull - NACA model 44 by Joe W. Bell
[Washington, DC]: NACA, [1936]

Zimmerman, Charles H. [VerfasserIn]
570: Effect of changes in tail arrangement upon the spinning of a low wing monoplane [model] by C. H. Zimmerman
[Washington, DC]: NACA, [1936]

MacAvoy, William H. [VerfasserIn]
555: Piloting technique for recovery from spins by W. H. McAvoy
[Washington, DC]: NACA, [1936]

Burgess, C. P. [VerfasserIn]
746: The frequencies of cantilever wings in beam and torsional vibration by C. P. Burgess
Washington, D.C.: NACA, 1936

Dearborn, Clinton H. [VerfasserIn]; Soulé, Hartley A. [VerfasserIn]
578: Full scale wind tunnel and flight tests of a Fairchild 22 airplane equipped with a Fowler flap by C. H. Dearborn and H. A. Soulé
Washington, D.C.: NACA, 1936

White, Roland J. [VerfasserIn]; Martin, Victor J. [VerfasserIn]
579: Charts for calculating the performance of airplanes having constant speed propellers by Roland J. White and Victor J. Martin
Washington, D.C.: NACA, 1936

Kuhn, Paul [VerfasserIn]
562: Remarks on the elastic axis of shell wings by Paul Kuhn
Washington, D.C.: NACA, 1936

Kuhn, Paul [VerfasserIn]
530: Bending stresses due to torsion in cantile[ver box beams] by Paul Kuhn
[Washington]: NACA, [1935]

Wetmore, J. W. [VerfasserIn]
568: Calculated effect of various types of flap on take-off over obstacles by J. W. Wetmore
[Washington, DC]: NACA, [1935]

Stack, John [VerfasserIn]
543: The compressibility burble by John Stack
[Washington, DC]: NACA, [1935]

Hartman, Edwin P. [VerfasserIn]
525: The aerodynamic drag of flying boat hull models as measured in the NACA 20-foot wind tunnel by Edwin P. Hartman
[Washington, DC]: NACA, [1935]

Bamber, Millard J. [VerfasserIn]; Zimmermann, C. H. [VerfasserIn]
517: The aerodynamic forces and moments on a spinning model of the F4B 2 airplane as measured by the spinning balance by J. B. Parkinson and J. W. Bell
Washington, D.C.: NACA, 1935

Lundquist, Eugene E. [VerfasserIn]
523: Strength tests of thin walled duralumin cylinders in combined transverse shear and bending by Eugene E. Lundquist
Washington, D.C.: NACA, 1935

Lundquist, Eugene E. [VerfasserIn]; Burke, Walter F. [VerfasserIn]
527: Strength tests of thin walled duralumin cylinders of elliptic section by Eugene E. Lundquist and Walter F. Burke
Washington, D.C.: NACA, 1935

Zimmerman, Charles H. [VerfasserIn]
539: Aerodynamic characteristics of several airfoils of low aspect ratio by C. H. Zimmerman
[Washington, DC]: NACA, [1935]

Soulé, Hartley A. [VerfasserIn]
548: Flight tests of a balanced split flap with particular reference to rapid operation by H. A. Soule
[Washington, DC]: NACA, [1935]

Bamber, Millard J. [Sonstige Person, Familie und Körperschaft]
526: Spinning characteristics of wings 2 Rectangular Clark Y biplane cellule: 25 percent stagger, 0 o decalage, gap/chord [1.0] / by M. J. Bamber by M. J. Bamber and C. H. Zimmerman
[Washington, DC]: NACA, 1935

Kuhn, Paul [VerfasserIn]
542: The initial torsional stiffness of shells with interior webs by Paul Kuhn
[Washington]: NACA, [1935]

529: Analysis of a strut with a single elastic support in the span 1 Derivation of formulas / by A. M. Schwartz by A. Murray Schwartz and Reid Bogert
[Washington, DC]: NACA, 1935

Weick, Fred E. [VerfasserIn]
552: Wind tunnel tests of wing flaps suitable for direct control of glide-fath angle by Fred E. Weick
[Washington, DC]: NACA, [1935]

Pearson, Henry A. [VerfasserIn]
571: A method of estimating the aerodynamic effects of ordinary and split flaps on airfoils similar to the Clark Y by H. A. Pearson
[Washington, DC]: NACA, [1935]

Weick, Fred E. [VerfasserIn]; Shortal, Joseph A. [VerfasserIn]
547: Development of the NACA slot lip [aileron] by Fred E. Weick and Joseph [A. Shortal]
[Washington, DC]: NACA, [1935]

Scudder, Nathan F. [VerfasserIn]
468: A study of factors affecting the steady spin of an airplane by Nathan F. Scudder
[Washington, DC]: NACA, [1935]

Jacobs, Eastman N. [VerfasserIn]; Pinkerton, Robert M. [VerfasserIn]
567: Tests of NACA airfoils in the variable density wind tunnel 230 Series 230 by Eastman N. Jacobs and Robert M. Pinkerton
Washington, D.C.: NACA, 1935

Parsons, John F. [VerfasserIn]
521: Full scale force and pressure distribution tests on a tapered U.S.A. 45 airfoil by John F. Parsons
Washington, D.C.: NACA, 1935

Noyes, Richard W. [VerfasserIn]
524: Wind tunnel tests of a wing with a trailing edge auxiliary airfoil used as a flap by Richard W. Noyes
Washington, D.C.: NACA, 1935

Hubbard, John D. [VerfasserIn]; Brescoll, George P. [VerfasserIn]
502: Aerodynamic investigation of a cup anemometer by John D. Hubbard and George P. Brescoll
Washington, D.C.: NACA, 1934

Hartman, Edwin P. [VerfasserIn]
484: A method of calculating the performance of controllable propellers, with sample computations by Edwin P. Hartman
Washington, D.C.: NACA, 1934

Higgins, George J. [VerfasserIn]
511: A study of the pitching moments and the stability characteristics of monoplanes by George J. Higgins
Washington, D.C.: NACA, 1934

Truscott, Starr [VerfasserIn]
513: The wave suppressors used in the N.A.C.A. tank by Starr Truscott
Washington, D.C.: NACA, 1934

Noyes, Richard W. [VerfasserIn]
524: Wind tunnel tests of a wing with a trailing edge auxiliary airfoil used as a flap by Richard W. Noyes
[Washington, DC]: NACA, [1934]

Kuhn, Paul [VerfasserIn]
500: The torsional stiffness of thin duralumin shells subjected to large torques by Paul Kuhn
Washington, D.C.: NACA, 1934

Dawson, John R. [VerfasserIn]
512: A complete tank test of the hull of the Sikorsky S 40 flying boat - American Clipper class by John R. Dawson
Washington, D.C.: NACA, 1934

Bamber, Millard J. [VerfasserIn]
515: Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model by J. M. Bamber
Washington, D.C.: NACA, 1934

Wenzinger, Carl J. [VerfasserIn]
505: The effects of full span and partial span split flaps on the aerodynamic characteristics of a tapered wing by Carl J. Wenzinger
Washington, D.C.: NACA, 1934

Sherman, Albert [VerfasserIn]; Harris, Thomas A. [VerfasserIn]
507: The effects of equal pressure fixed slots on the characteristics of a clark y airfoil by Albert Sherman and Thomas A. Harris
Washington, D.C.: NACA, 1934

Peck, William C. [VerfasserIn]
508: Landing characteristics of an autogiro by William C. Peck
[Washington, DC]: NACA, [1934]

Schliestett, George van [VerfasserIn]
506: Experimental verification of Theodorsen's theoretical jet boundary correction factors by George Van Schliestett
Washington, D.C.: NACA, 1934

Brevoort, Maurice J. [VerfasserIn]
501: Landing shock recorder by Maurice J. Brevoort
[Washington, DC]: NACA, 1934

DeFrance, Smith J. [VerfasserIn]
495: Effect of the surface condition of a wing on the aerodynamic characteristics of an airplane by S. J. DeFrance
[Washington, DC]: NACA, [1934]

Wenzinger, Carl J. [VerfasserIn]
498: Wind tunnel measurements of air loads on split flaps by Carl J. Wenzinger
Washington, D.C.: NACA, 1934

Brombacher, William G. [VerfasserIn]
503: Measurement of altitude in blind flying by W. G. Brombacher
Washington, D.C.: NACA, 1934

Shortal, Joseph A. [VerfasserIn]
499: Effect of retractable spoiler location on rolling and yawing moment coefficients by J. A. Shortal
[Washington, DC]: NACA, [1934]

Dearborn, Clinton H. [VerfasserIn]
497: Full scale drag tests of landing lamps by C. H. Dearborn
Washington, D.C.: NACA, 1934

Shoemaker, James M. [VerfasserIn]
509: Thank tests of flat and V bottom planing surfaces by James M. Shoemaker
Washington, D.C.: NACA, 1934

Parkinson, John B. [VerfasserIn]; Bell, Joe W. [VerfasserIn]
510: The calculated effect of trailing edge flaps on the take off of flying boats by J. B. Parkinson and J. W. Bell
Washington, D.C.: NACA, 1934

494: Hazards to aircraft due to electrical phenomena report of the Special Committee on Hazards to Aircraft due to Electrical Phenomena
[Washington, DC]: NACA, [1934]

Lundquist, Eugene E. [VerfasserIn]
479: Strength test of thin walled duralu[min cylinders] in pure bending by Eugene E. Lundquist
[Washington, DC]: NACA, [1933]

Weick, Fred E. [Sonstige Person, Familie und Körperschaft]; Harris, Thomas A. [Sonstige Person, Familie und Körperschaft]
458: Wind tunnel resarch comparing lateral control devices, particularly at high angles of attack 11 Various floating tip ailerons on both rectangular and tapered wings / by Fred E. Weick and Tomas A. Harris
Washington, D.C.: NACA, 1933

Marsh, Edred T. [VerfasserIn]; Waldron, C. D. [VerfasserIn]
465: Some characteristics of sprays obtained from pintle type injection nozzles by E. T. Marsh and C. D. Waldron
Washington, D.C.: NACA, 1933

Anderson, Raymond F. [VerfasserIn]
487: Tests of three tapered airfoils based on the NACA 2200, the NACA-M6, and the Clark Y by Raymond F. Anderson
[Washington, DC]: NACA, [1933]

Jacobs, Eastman N. [VerfasserIn]
481: The reduction in drag of a forward sloping windshield by Eastman N. Jacobs
[Washington, DC]: NACA, [1933]

Heald, R. H. [VerfasserIn]
441: Rolling, yawing, and hinge moments produced by rectangular ailerons (correlating technical reports nos. 298, 343, and 370) by R. H. Heald
Washington, D.C.: NACA, 1933

Schubauer, Galen B. [VerfasserIn]
442: Jet propulsion with special reference to thrust augmentors by G. B. Schubauer
Washington, D.C.: NACA, 1933

Weick, Fred E. [Sonstige Person, Familie und Körperschaft]; Wenzinger, Carl J. [Sonstige Person, Familie und Körperschaft]
449: Wind tunnel resarch comparing lateral control devices, particularly at high angles of attack 9 Tapered wings with ordinary ailerons / by Fred E. Weick and Carl J. Wenzinger
Washington, D.C.: NACA, 1933

Lesley, E. P. [VerfasserIn]
453: Experiments with a counter propeller by E. P. Lesley
Washington, D.C.: NACA, 1933

Shoemaker, James M. [VerfasserIn]
471: A complete tank test of a model of a flying boat hull - N.A.S.A. model 16 by James M. Shoemaker
Washington, D.C.: NACA, 1933

Soulé, Hartley A. [VerfasserIn]; Wetmore, J. W. [VerfasserIn]
478: The effect of slots and flaps on lateral control of a low wing monoplane as determined in flight by Hartley A. Soulé and J. W. Wetmore
Washington, D.C.: NACA, 1933

Anderson, Raymond F. [VerfasserIn]
483: Charts for determining the pitching moment of tapered wings with sweepback and twist by Raymond F. Anderson
Washington, D.C.: NACA, 1933

Wheatley, John B. [VerfasserIn]
467: Simplified aerodynamic analysis of the cyclogiro rotating wing sys[tem] by John B. Wheatley
[Washington, DC]: NACA, [1933]

Jacobs, Eastman N. [VerfasserIn]
480: The drag of streamline wires by Eastman N. Jacobs
[Washington, DC]: NACA, [1933]

Parkinson, John B. [VerfasserIn]
470: A complete tank test of a model of a flying boat hull N.A.C.A. model No. 11-A by John B. Parkinson
Washington, D.C.: NACA, 1933

Hocker, Ray W. [VerfasserIn]
457: The aerodynamic characteristics of airfoils as affected by surface roughness by Ray W. Hocker
Washington, D.C.: NACA, 1933

Weick, Fred E. [VerfasserIn]; Platt, Robert C. [VerfasserIn]
459: Wind tunnel tests on model wing with fowler flap and specially developed leading edge slot by Fred E. Weick and Robert C. Platt
[Washington, DC]: NACA, 1933

Shoemaker, James M. [VerfasserIn]; Parkinson, John B. [VerfasserIn]
464: A complete tank test of a model of a flying boat hull - N.A.S.A. model no. 11 by James M. Shoemaker and John B. Parkinson
Washington, D.C.: NACA, 1933

Wenzinger, Carl J. [VerfasserIn]
472: The effect of partial span split flaps on the aerodynamic characteristics of a Clark Y wing by Carl J. Wenzinger
Washington, D.C.: NACA, 1933

Schey, Oscar W. [VerfasserIn]; Young, Alfred W. [VerfasserIn]
466: Engine performance with a hydrogenated safety fuel by Oscar W. Schey and Alfred W. Young
Washington, D.C.: NACA, 1933

Wallace, Rudolf N. [VerfasserIn]
475: The effect of split trailing edge wing flaps on the aerodynamic characteristics of a parasol monoplane by Rudolf N. Wallace
[Washington, DC]: NACA, [1933]

Wheatley, John B. [VerfasserIn]; Windler, Ray [VerfasserIn]
528: Wind tunnel tests of a cyclogiro rotor by John B. Wheatley and Ray Windler
[Washington, DC]: NACA, [1933]

Ober, Shatswell [VerfasserIn]
446: Estimation of the variation of thrust horsepower with air speed by Shatswell Ober
Washington, D.C.: NACA, 1933

Weick, Fred E. [Sonstige Person, Familie und Körperschaft]; Shortal, Joseph A. [Sonstige Person, Familie und Körperschaft]
445: Wind tunnel resarch comparing lateral control devices, particularly at high angles of attack 8 Straight and skewed ailerons on wings with rounded tips / by Fred E. Weick and Joseph A. Shortal
Washington, D.C.: NACA, 1933

Weick, Fred E. [Sonstige Person, Familie und Körperschaft]; Wenzinger, Carl J. [Sonstige Person, Familie und Körperschaft]
443: Wind tunnel resarch comparing lateral control devices, particularly at high angles of attack 7 Handley page tip and full-span slots with ailerons and spoilers / by Fred E. Weick and Carl J. Wenzinger
Washington, D.C.: NACA, 1933

Weick, Fred E. [VerfasserIn]; Scudder, Nathan F. [VerfasserIn]
447: The effect on lift, drag, and spinning characteristics of sharp leading edges on airplane wings by Fred E. Weick and Nathan F. Scudder
Washington, D.C.: NACA, 1933

Heald, R. H. [VerfasserIn]
448: Effect of aileron displacement on wing characteristics by R. H. Heald
Washington, D.C.: NACA, 1933

Weick, Fred E. [Sonstige Person, Familie und Körperschaft]; Noyes, Richard W. [Sonstige Person, Familie und Körperschaft]
451: Wind tunnel resarch comparing lateral control devices, particularly at high angles of attack 10 Various control devices on a wing with a fixed auxiliary airfoil / by Fred E. Weick and Richard W. Noyes
Washington, D.C.: NACA, 1933

Wilkie, J. B. [VerfasserIn]
450: Mercerization of cotton for strength with special reference to aircraft cloth by J. B. Wilkie
Washington, D.C.: NACA, 1933

Taylor, Edward S. [VerfasserIn]
452: The importance of auto ignition lag in knocking by E. S. Taylor
Washington, D.C.: NACA, 1933

Spanogle, J. A. [VerfasserIn]; Buckley, E. C. [VerfasserIn]
454: The N.A.C.A. combustion chamber gas sampling valve and some preliminary test results by J. A. Spanogle and E. C. Buckley
Washington, D.C.: NACA, 1933

Lundquist, Eugene E. [VerfasserIn]
455: Comparison of three methods for calculating the compressive strength of flat and slightly curved sheet and stiffener combinations by Eugene E. Lundquist
Washington, D.C.: NACA, 1933

DeFrance, Smith J. [VerfasserIn]
456: The aerodynamic effect of a retractable landing gear by Smith J. DeFrance
Washington, D.C.: NACA, 1933

Hood, Manley J. [VerfasserIn]; White, James A. [VerfasserIn]
460: Full scale wind tunnel research on tail buffeting and wing fuselage interference of a low-wing monoplane by Manley J. Hood and James A. White
Washington, D.C.: NACA, 1933

Weick, Fred E. [VerfasserIn]; Sanders, Robert [VerfasserIn]
463: Aerodynamic tests of low aspect ratio tapered wing with various flaps, for use tailless airplanes by Fred E. Weick and Robert Sanders
Washington, D.C.: NACA, 1933

Bamber, Millard J. [VerfasserIn]
474: Effect of stabilizer [...] by M. J. Bamber
[Washington, D.C.]: NACA, [ca. 1933]

Sanders, Robert [VerfasserIn]
477: Aerodynamic tests of a low aspect ratio tapered wing with an auxiliary airfoil for use tailless airplanes by Robert Sanders
Washington, D.C.: NACA, 1933

Dearborn, Clinton H. [VerfasserIn]
461: The effect of rivet heads on the characteristics of a 6 by 36 foot clark Y metal airfoil by Clinton H. Dearborn
Washington, D.C.: NACA, 1933

Taylor, Edward S. [VerfasserIn]
405: Valve timing of engines having intake pressures higher than exhaust by Edward S. Taylor
Washington, D.C.: NACA, 1932

Weick, Fred E. [VerfasserIn]; Wenzinger, Carl J. [VerfasserIn]
423: Effect of length of handley page tip slots on the lateral stability factor, damping in roll by Fred E. Weick and Carl J. Wenzinger
Washington, D.C.: NACA, 1932

Rothrock, A. M. [VerfasserIn]; Lee, Dana W. [VerfasserIn]
407: Effect of the reservoir volume on the discharge pressures in the injection system of the N.A.C.A. spray photography equipment by A. M. Rothrock and D. W. Lee
Washington, D.C.: NACA, 1932

Lundquist, Eugene E. [VerfasserIn]
427: Strength tests on thin walled duralumin cylinders in torsion by Eugene E. Lundquist
Washington, D.C.: NACA, 1932

Schey, Oscar W. [VerfasserIn]; Biermann, Arnold E. [VerfasserIn]
429: Heat dissipation from a finned cylinder at different fin plane air stream angles by Oscar W. Schey and Arnold E. Biermann
Washington, D.C.: NACA, 1932

Rothrock, A. M. [VerfasserIn]; Waldron, C. D. [VerfasserIn]
430: Effect of engine operating conditions on the vaporization of safety fuels by A. M. Rothrock and C. D. Waldron
Washington, D.C.: NACA, 1932

Gerrish, Harold C. [VerfasserIn]; Voss, Fred [VerfasserIn]
434: Influence of several factors on ignition lag in a compression ignition engine by Harild C. Gerrish and Fred Voss
Washington, D.C.: NACA, 1932

Stevens, F. W. [VerfasserIn]
438: The gaseous explosive reaction at constant pressure - further data on the effect of inert gases by F. W. Stevens
Washington, D.C.: NACA, 1932

Weick, Fred E. [VerfasserIn]; Sanders, Robert [VerfasserIn]
417: Wind tunnel tests of a hall high lift wing by Fred E. Weick and Robert Sanders
Washington, D.C.: NACA, 1932

Lee, Dana W. [VerfasserIn]; Spencer, Robert C. [VerfasserIn]
424: Preliminary photomicrographic studies of fuel sprays by Dana W. Lee and Robert C. Spencer
Washington, D.C.: NACA, 1932

Weick, Fred E. [VerfasserIn]; Harris, Thomas A. [VerfasserIn]
422: The aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear by Fred E. Weick and Thomas A. Harris
Washington, D.C.: NACA, 1932

Scudder, Nathan F. [VerfasserIn]; Miller, Marvel P. [VerfasserIn]
421: The nature of air flow about the tail of an airplane in a spin by N. F. Scudder and M. P. Miller
Washington, D.C.: NACA, 1932

Gough, Melvin N. [VerfasserIn]; Johnson, Ernest [VerfasserIn]
425: Methods of visually determining the air flow around airplanes by Melvin N. Gough and Ernest Johnson
[Washington, DC]: NACA, [1932]

Rothrock, A. M. [VerfasserIn]
408: Preliminary tests on the vaporization of fuel sprays by A. M. Rothrock
Washington, D.C.: NACA, 1932

Lee, Dana W. [VerfasserIn]
410: Experiments on the distribution of fuel in fuel sprays by Dana W. Lee
Washington, D.C.: NACA, 1932

Ward, Kenneth E. [VerfasserIn]
428: Characteristics of an airfoil as affected by fabric sag by Kenneth E. Ward
[Washington, DC]: NACA, [1932]

Moore, Charles S. [VerfasserIn]; Collins, John H. [VerfasserIn]
435: The effect of clearance distribution on the performance of a compression ignition engines with a precombustion chamber by C. S. Moore and J. H. Collins
Washington, D.C.: NACA, 1932

Moore, Charles S. [VerfasserIn]; Collins, John H. [VerfasserIn]
436: The effect of connecting passage diameter on the performance of a compression ignition engine with a precombustion chamber by C. S. Moore and J. H. Collins
Washington, D.C.: NACA, 1932

Spanogle, J. A. [VerfasserIn]
418: Compression ignition engine tests of several fuels by J. A. Spanogle
Washington, D.C.: NACA, 1932

Weick, Fred E. [VerfasserIn]; Platt, Robert C. [VerfasserIn]
419: Wind tunnel tests of the fowler variable area wing by Fred E. Weick and Robert C. Platt
Washington, D.C.: NACA, 1932

Spanogle, J. A. [VerfasserIn]; Moore, Charles S. [VerfasserIn]
414: Considerations of air flow in combustion chambers of high speed compression ignition engines by J. A. Spanogle and C. S. Moore
Washington, D.C.: NACA, 1932

Anderson, Raymond F. [VerfasserIn]
412: The aerodynamic characteristics of airfoils at negative angles of attack by Raymond F. Anderson
Washington, D.C.: NACA, 1932

Soulé, Hartley A. [VerfasserIn]
440: Flight tests to determine the effect of a fixed auxiliary airfoil on the lift and drag of a parasol monoplane by Hartley A. Soulé
Washington, D.C.: NACA, 1932

Schey, Oscar W. [VerfasserIn]; Ellerbrock, Herman H. [VerfasserIn]
426: Comperative performance of a powerplus vane type supercharger and an N.A.S.A. roots type supercharger by Oscar W. Schey and Herman H. Ellerbrock
Washington, D.C.: NACA, 1932

Windler, Ray [VerfasserIn]
432: Drag tests of 4 9 scale model engine nacelles with various cowlings by Ray Windler
Washington, D.C.: NACA, 1932

Rhode, Richard V. [VerfasserIn]
433: The pressure distribution over a standard and a modified Navy elliptical wing tip on a biplane in flight by Richard V. Rhode
Washington, D.C.: NACA, 1932

Weick, Fred E. [VerfasserIn]; Wenzinger, Carl J. [VerfasserIn]
415: Preliminary investigation of rolling moments obtained with spoilers on both slotted and plain wings by Fred E. Weick and Carl J. Wenzinger
Washington, D.C.: NACA, 1932

Burke, Walter F. [VerfasserIn]
444: Working charts for the stress analysis [of elliptic rings] by Walter F. Burke
[Washington, DC]: NACA, 1932

Windler, Ray [VerfasserIn]
420: The effect of propellers and nacelles on the landing speeds of tractor monoplanes by Ray Windler
Washington, D.C.: NACA, 1932

Lundquist, Eugene E. [VerfasserIn]
413: The compressive strength of duralumin columns of equal angle section by Eugene E. Lundquist
Washington, D.C.: NACA, 1932

Schey, Oscar W. [VerfasserIn]; Young, Alfred W. [VerfasserIn]
406: The use of large valve overlap in scavenging a supercharged spark ignition engine using fuel injection by Oscar W. Schey and Alfred W. Young
Washington, D.C.: NACA, 1932

Rhode, Richard V. [VerfasserIn]
437: The pressure distribution over a long elliptical wing tip on a biplane in flight by Richard V. Rhode
Washington, D.C.: NACA, 1932

Samuels, L. T. [VerfasserIn]
439: Meteorological conditions during the formation of ice on aircraft by L. T. Samuels
Washington, D.C.: NACA, 1932

Jacobs, Eastman N. [VerfasserIn]; Ward, Kenneth E. [VerfasserIn]
404: Tests of NACA airfoils in the variable density wind tunnel series 24 by Eastman N. Jacobs and Kenneth E. Ward
Washington, D.C.: NACA, 1932

Theodorsen, Theodore [VerfasserIn]; Clay, William C. [VerfasserIn]
394: The prevention of ice formation on gasoline tank vents by Theodore Theodorsen and William C. Clay
Washington, D.C.: NACA, 1931

Spanogle, J. A. [VerfasserIn]; Whitney, E. G. [VerfasserIn]
403: The effectiveness of a double stem injection valve in controlling combustion in a compression ignition engine by J. A. Spanogle and E. G. Whitney
Washington, D.C.: NACA, 1931

Ward, Kenneth E. [VerfasserIn]
403: The interference effects on an airfoil of a flat plate at mid span position by Kenneth E. Ward
Washington, D.C.: NACA, 1931

Taylor, Charles Fayette [VerfasserIn]
380: A suggested method for measuring turbulence by C. Fayette Taylor
Washington, D.C.: NACA, 1931

Swickard, Andrew E. [VerfasserIn]
383: Metal truss wing spars by Andrew E. Swickard
Washington, D.C.: NACA, 1931

Spanogle, J. A. [VerfasserIn]; Foster, Hampton H. [VerfasserIn]
382: Basic requirements of fuel injection nozzles for quiescent combustion chambers by J. A. Spanogle and H. H. Foster
Washington, D.C.: NACA, 1931

Russell, H. W. [VerfasserIn]; Welcker, W. A. [VerfasserIn]
381: Endurance and other properties at low temperatures of some alloys for aircraft use by H. W. Russell and W. A. Welcker
Washington, D.C.: NACA, 1931

Miller, Marvel P. [VerfasserIn]; Soulé, Hartley A. [VerfasserIn]
375: Moments of inertia of airplanes by Marvel P. Miller and Hartley A. Soulé
Washington, D.C.: NACA, 1931

Rhode, Richard V. [VerfasserIn]; Lundquist, Eugene E. [VerfasserIn]
387: The pressure distribution over a modified elliptical wing tip on a biplane in flight by Richard V. Rhode and Eugene E. Lundquist
Washington, D.C.: NACA, 1931

Jacobs, Eastman N. [VerfasserIn]
416: Characteristics of two sharp nosed airfoils having reduced spinning tendencies by Eastman N. Jacobs
[Washington, DC]: NACA, [1931]

Ward, Kenneth E. [VerfasserIn]
365: Interference effects and drag of struts on a monoplane wing by Kenneth E. Ward
Washington, D.C.: NACA, 1931

Hartmann, E. C. [VerfasserIn]
378: Comparison of weights of 17ST and steel tubular structural members used in aircraft construction by E. C. Hartmann
Washington, D.C.: NACA, 1931

Miller, Roy A. [VerfasserIn]; Wood, K. D. [VerfasserIn]
462: Formulas for the stress analysis of circular rings in a monocoque fuselage by Roy A. Miller and Karl D. Wood
[Washington, D.C.]: NACA, [ca. 1931]

Pinkerton, Robert M. [VerfasserIn]
386: Effect of nose shape on characteristics of symmetrical airfoils by Robert M. Pinkerton
Washington, D.C.: NACA, 1931

DeFoe, George L. [VerfasserIn]
388: A comparison of the aerodynamic characteristics of three normal and three reflexed airfoils in the variable density wind tunnel by George L. Defoe
Washington, D.C.: NACA, 1931

Ward, Kenneth E. [VerfasserIn]
361: The effect of small variations in profile of airfoils by Kenneth E. Ward
Washington, D.C.: NACA, 1931

Anderson, Raymond F. [VerfasserIn]
367: The aerodynamic characteristics of three tapered airfoils tested in the variable density wind tunnel by John B. Wheatley
Washington, D.C.: NACA, 1931

Gough, Melvin N. [VerfasserIn]
368: The variation in pressure in the cabin of an airplane in flight by Melvin N. Gough
Washington, D.C.: NACA, 1931

Rothrock, A. M. [VerfasserIn]; Marsh, Edred T. [VerfasserIn]
384: The effect of injection valve opening pressure on spray tip penetration by A. M. Rothrock and E. T. Marsh
Washington, D.C.: NACA, 1931

Gelalles, A. G. [VerfasserIn]; Marsh, Edred T. [VerfasserIn]
369: Effect of orifice length diameter ratio on the coefficient of discharge of fuel injection nozzles by A. G. Gelalles and E. T. Marsh
Washington, D.C.: NACA, 1931

Jacobs, Eastman N. [VerfasserIn]
385: Tests of six symmetrical airfoils in the variable density wind tunnel by Easrman N. Jacobs
Washington, D.C.: NACA, 1931

Schey, Oscar W. [VerfasserIn]; Young, Alfred W. [VerfasserIn]
390: A method for reducing the temperature of exhaust manifolds by Oscar W. Schey and Alfred W. Young
Washington, D.C.: NACA, 1931

Thompson, F. L. [VerfasserIn]; Keister, P. H. [VerfasserIn]
362: Lift and drag characteristics of a cabin monoplane determined in flight by F. L. Thompson and P. H. Keister
Washington, D.C.: NACA, 1931

Weick, Fred E. [VerfasserIn]
363: The behavior of conventional airplanes in situations thought to lead to most crashes by Fred E. Weick
Washington, D.C.: NACA, 1931

Stack, John [VerfasserIn]
364: Tests in the variable density wind tunnel to investigate the effects of scale and turbulence on airfoil characteristics by John Stack
Washington, D.C.: NACA, 1931

Wheatley, John B. [VerfasserIn]
366: Torsion in box wings by John B. Wheatley
Washington, D.C.: NACA, 1931

Soulé, Hartley A. [VerfasserIn]
398: The effect of slots and flaps on the lift and drag of the Mcdonnell airplane as determined in flight by Hartley A. Soulé
Washington, D.C.: NACA, 1931

Rhode, Richard V. [VerfasserIn]; Lundquist, Eugene E. [VerfasserIn]
379: The pressure distribution over a semicircular wing tip on a biplane in flight by Richard V. Rhode and Eugene E. Lundquist
Washington, D.C.: NACA, 1931

Rhode, Richard V. [VerfasserIn]; Lundquist, Eugene E. [VerfasserIn]
360: The pressure distribution over a square wing tip on a biplane in flight by Richard V. Rhode and Eugene E. Lundquist
Washington, D.C.: NACA, 1931

Appel, Wm. D. [VerfasserIn]; Worner, Ruby K. [VerfasserIn]
393: An investigation of cotton for parachute cloth by Wm. D. Appel and R. K. Worner
Washington, D.C.: NACA, 1931

Anderson, Raymond F. [VerfasserIn]
397: The aerodynamic characteristics of six commonly used airfoils over a large range of positive and negative angles of attack by Raymond F. Anderson
Washington, D.C.: NACA, 1931

Jacobs, Eastman N. [VerfasserIn]; Pinkerton, Robert M. [VerfasserIn]
401: Tests of NACA airfoils in the variable density wind tunnel 44/64 Series 44 and 64 by Eastman N. Jacobs and Robert M. Pinkerton
Washington, D.C.: NACA, 1931

Rothrock, A. M. [VerfasserIn]
389: The NACA apparatus for studying the formation and combustion of fuel sprays and the results from preliminary tests by A. M. Rothrock
Washington, D.C.: NACA, 1931

Noyes, Richard W. [VerfasserIn]
377: An integrating manometer for use in wind tunnel pressure distribution measurements by Richard W. Noyes
Washington, D.C.: NACA, 1931

Spanogle, J. A. [VerfasserIn]; Moore, Charles S. [VerfasserIn]
396: Performance of a compression ignition engine with a precombustion chamber having high velocity air flow by J. A. Spanogle and C. S. Moore
Washington, D.C.: NACA, 1931

Jacobs, Eastman N. [VerfasserIn]; Pinkerton, Robert M. [VerfasserIn]
391: Tests of NACA airfoils in the variable density wind tunnel 43/63 Series 43 and 63 by Eastman N. Jacobs and Robert M. Pinkerton
Washington, D.C.: NACA, 1931

Jacobs, Eastman N. [VerfasserIn]; Pinkerton, Robert M. [VerfasserIn]
392: Tests of NACA airfoils in the variable density wind tunnel 45/65 Series 45 and 65 by Eastman N. Jacobs and Robert M. Pinkerton
Washington, D.C.: NACA, 1931

Rothrock, A. M. [VerfasserIn]; Marsh, Edred T. [VerfasserIn]
395: Penetration and duration of fuel sprays from pump injection system by A. M. Rothrock and E. T. Marsh
Washington, D.C.: NACA, 1931

Rothrock, A. M. [VerfasserIn]; Waldron, C. D. [VerfasserIn]
399: Some characteristics of fuel sprays at low injection pressures by A. M. Rothrock and C. D. Waldron
Washington, D.C.: NACA, 1931

Rothrock, A. M. [VerfasserIn]
376: Effect of high air velocities on the distribution and penetration of a fuel spray by A. M. Rothrock
Washington, D.C.: NACA, 1931

Miller, Marvel P. [VerfasserIn]
351: An accurate method of measuring the moments of inertia of airplanes by M. P. Miller
Washington, D.C.: NACA, 1930

Mossman, Ralph W. [VerfasserIn]; Robinson, Russell G. [VerfasserIn]
357: Bending tests of metal monocoque fuselage construction by Ralph W. Mossman and Russell G. Robinson
Washington, D.C.: NACA, 1930

Gelalles, A. G. [VerfasserIn]
352: Effect of orifice length diameter ratio on spray characteristics by A. G. Gelalles
Washington, D.C.: NACA, 1930

Gough, Melvin N. [VerfasserIn]
355: Effect of the angular position of the section of a ring cowling on the high speed of an XF7C 1 airplane by Melvin N. Gough
Washington, D.C.: NACA, 1930

Geer, William C. [VerfasserIn]; Scott, Merit [VerfasserIn]
345: The prevention of the ice hazard on airplanes by William C. Geer and Merit Scott
Washington, D.C.: NACA, 1930

Lesley, E. P. [VerfasserIn]
333: Test of an adjustable pitch model propeller at four blade settings by E. P. Lesley
Washington, D.C.: NACA, 1930

Rhode, Richard V. [VerfasserIn]; Lundquist, Eugene E. [VerfasserIn]
347: The pressure distribution over a Douglas wing tip on a biplane in flight by Richard V. Rhode and Eugene E. Lundquist
Washington, D.C.: NACA, 1930

Schey, Oscar W. [VerfasserIn]; Johnson, Ernest [VerfasserIn]; Gough, Melvin N. [VerfasserIn]
334: Comparative performance obtained with XF7C 1 airplane using several different engine cowlings by Oscar W. Schey; Ernest Johnson and Melvin N. Gough
Washington, D.C.: NACA, 1930

Mutchler, W. H. [VerfasserIn]; Buzzard, Robert Walton [VerfasserIn]
350: Methods for the identification of aircraft tubing of plain carbon steel and chromium molybdenum steel by W. H. Mutchler and R. W. Buzzard
Washington, D.C.: NACA, 1930

McNicholas, Harry J. [VerfasserIn]; Hedrick, Anna F. [VerfasserIn]
335: The structure and properties of parachute cloths by H. J. McNicholas and A. F. Hedrick
Washington, D.C.: NACA, 1930

Rothrock, A. M. [VerfasserIn]
332: Injection lags in a common rail fuel injection system by A. M. Rothrock
Washington, D.C.: NACA, 1930

Knight, Montgomery [VerfasserIn]; Wenzinger, Carl J. [VerfasserIn]
336: The effect of wing tip floating ailerons on the autorotation of a monoplane wing model by Montgomery Knight and Carl J. Wenzinger
Washington, D.C.: NACA, 1930

Taylor, Charles Fayette [VerfasserIn]; Rehbock, A. [VerfasserIn]
331: Rate of heat transfer from finned metal surfaces progress report on investigations at Aeronautical Engineering Department, Massachusetts Institute of Technology by C. Fayette Taylor and A. Rehbock
Washington, D.C.: NACA, 1930

Collins, John H. [VerfasserIn]
348: Alterations and tests of the "Farnboro" engine indicator by John H. Collins
Washington, D.C.: NACA, 1930

Rothrock, A. M. [VerfasserIn]; Lee, Dana W. [VerfasserIn]
356: Some characteristics of fuel sprays from open nozzles by A. M. Rothrock and D. W. Lee
Washington, D.C.: NACA, 1930

Knerr, Horace [VerfasserIn]
342: Identification of aircraft tubing by rockwell test by Horace Knerr
Washington, D.C.: NACA, 1930

Spanogle, J. A. [VerfasserIn]; Foster, Hampton H. [VerfasserIn]
344: Performance of a high speed compression ignition engine using multiple orifice fuel injection nozzles by J. A. Spanogle and H. H. Foster
Washington, D.C.: NACA, 1930

Rhode, Richard V. [VerfasserIn]
337: Pressure distribution on the tail surfaces of a PW-9 pursuit airplane in flight by Richard V. Rhode
Washington, D.C.: NACA, 1930

Pinkerton, Robert M. [VerfasserIn]
353: Analytical determination of the load on a trailing dege flap by Robert M. Pinkerton
Washington, D.C.: NACA, 1930

Ridley, Kenneth F. [VerfasserIn]
349: An investigation of airplane landing speeds by Kenneth F. Ridley
Washington, D.C.: NACA, 1930

Gelalles, A. G. [VerfasserIn]
338: Some effects of air and fuel oil temperatures on spray penetration and dispersion by A. G. Gelalles
Washington, D.C.: NACA, 1930

Schey, Oscar W. [VerfasserIn]
328: The effect of fuel consumption on cylinder temperatures and performance of a cowled wright J-5 engine by Oscar W. Schey
Washington, D.C.: NACA, 1929

Carroll, Thomas [VerfasserIn]; MacAvoy, William H. [VerfasserIn]
313: The formation of ice upon airplanes in flight by Thomas Carroll and William H. MacAvoy
Washington, D.C.: NACA, 1929

Rothrock, A. M. [VerfasserIn]; Beardsley, E. G. [VerfasserIn]
329: Some effects of air flow on the penetration and distribution of oil sprays by A. M. Rothrock and E. G. Beardsley
Washington, D.C.: NACA, 1929

Knight, Montgomery [VerfasserIn]; Bamber, Millard J. [VerfasserIn]
316: Wind tunnel tests on a model of a monoplane wing with floating allerons by Montgomery Knight and Millard J. Bamber
Washington, D.C.: NACA, 1929

Weick, Fred E. [VerfasserIn]
317: Tests of four racing type airfoils in the twenty-foot propeller research tunnel by Fred E. Weick
Washington, D.C.: NACA, 1929

Lesley, E. P. [VerfasserIn]; Reid, Elliott G. [VerfasserIn]
302: A new method for the prediction of airplane performance by E. P. Lesley and E. G. Reid
Washington, D.C.: NACA, 1929

Knight, Montgomery [VerfasserIn]; Noyes, Richard W. [VerfasserIn]
310: Wind tunnel pressure distribution tests on a series of biplane wing models 1 Effects of changes in stagger and gap by Montgomery Knight and Richard W. Noyes
Washington, D.C.: NACA, 1929

Hersey, Mayo D. [VerfasserIn]
315: Viscosity of diesel engine fuel oil under pressure by Mayo D. Hersey
Washington, D.C.: NACA, 1929

Weick, Fred E. [VerfasserIn]
318: Full scale investigation of the drag of a wing radiator by Fred E. Weick
Washington, D.C.: NACA, 1929

Knight, Montgomery [VerfasserIn]; Noyes, Richard W. [VerfasserIn]
330: Wind tunnel pressure distribution tests on a series of biplane wing models 3 Effects of changes in various combinations of stagger, gap, sweepback, and decalage by Montgomery Knight and Richard W. Noyes
Washington, D.C.: NACA, 1929

Von Kármán, Theodore [VerfasserIn]
321: The impact on seaplane floats during landing by Th. von Karman
Washington, D.C.: NACA, 1929

Weick, Fred E. [VerfasserIn]; Wood, Donald H. [VerfasserIn]
322: The effect of the wings of single engine airplanes on propulsive efficiency as shown by full scale wind tunnel tests by Fred E. Weick and Donald H. Wood
Washington, D.C.: NACA, 1929

Ross, Orrin E. [VerfasserIn]
306: Curves showing column strength of steel and duralumin tubing by Orrin E. Ross
Washington, D.C.: NACA, 1929

Jacobs, Eastman N. [VerfasserIn]
308: Pressure distribution on a slotted R.A.F. 31 airfoil in the varable density wind tunnel by Eastman N. Jacobs
Washington, D.C.: NACA, 1929

Carroll, Thomas [VerfasserIn]; MacAvoy, William H. [VerfasserIn]
314: Spiral tendency in blind flying by Thomas Carroll and William H. MacAvoy
Washington, D.C.: NACA, 1929

Ober, Shatswell [VerfasserIn]
319: Some experiments on autorotation of an airfoil by Shatswell Ober
Washington, D.C.: NACA, 1929

Jacobs, Eastman N. [VerfasserIn]
320: The drag and interference of a nacelle in the presence of a wing by Eastman N. Jacobs
Washington, D.C.: NACA, 1929

Knight, Montgomery [VerfasserIn]; Noyes, Richard W. [VerfasserIn]
325: Wind tunnel pressure distribution tests on a series of biplane wing models 2 Effects of changes in decalage, dihedral, sweepback and overhang by Montgomery Knight and Richard W. Noyes
Washington, D.C.: NACA, 1929

Wenzinger, Carl J. [VerfasserIn]; Loeser, Oscar [VerfasserIn]
326: Wind tunnel pressure distribution tests on an airfoil with trailling edge flap by Carl J. Wenzinger and Oscar Loeser
Washington, D.C.: NACA, 1929

Tuckerman, Louis B. [VerfasserIn]; Petrenko, Serge N. [VerfasserIn]; Johnson, C. D. [VerfasserIn]
307: Strength of tubing under combined axial and transverse loading by L. B. Tuckerman; S. N. Petrenko and C. D. Johnson
Washington, D.C.: NACA, 1929

Fliedner, C. S. [VerfasserIn]
303: Condensed data on the aircraft engines of the world compiled by C. S. Fliedner
Washington, D.C.: NACA, 1929

Ober, Shatswell [VerfasserIn]
327: Some studies on the aerodynamic effect of the gap between airplane wings and fuselages by Shatswell Ober
Washington, D.C.: NACA, 1929

Rawdon, Henry S. [VerfasserIn]
304: Corrosion embrittlement of duralumin 5 The results of weather exposure tests by Henry S. Rawdon
Washington, D.C.: NACA, 1929

Knight, Montgomery [VerfasserIn]; Bamber, Millard J. [VerfasserIn]
323: Wind tunnel tests on airfoil boundary layer control using a backward opening slot by Montgomery Knight and Millard J. Bamber
Washington, D.C.: NACA, 1929

DeFoe, George L. [VerfasserIn]
279: Resistance of streamline wires by George L. DeFoe
Washington, D.C.: NACA, 1928

Reid, Elliott G. [VerfasserIn]; Bamber, Millard J. [VerfasserIn]
286: Preliminary investigation on boundary layer control by means of suction and pressure with the U.S.A. 27 airfoil by E. G. Reid and M. J. Bamber
Washington, D.C.: NACA, 1928

Shoemaker, James M. [VerfasserIn]
289: Preliminary biplane tests in the variable density wind tunnel by James M. Shoemaker
Washington, D.C.: NACA, 1928

Knight, Montgomery [VerfasserIn]; Bamber, Millard J. [VerfasserIn]
297: Preliminary report on the flat top lift curve as a factor in control at low speed by Montgomery Knight and Millard J. Bamber
Washington, D.C.: NACA, 1928

Jones, Bennett Melvill [VerfasserIn]
485: Research on the control of airplanes by B. Melvill Jones
Washington, D.C.: NACA, 1928

Miller, W. B. [VerfasserIn]
290: Welding of high chromium steels by W. B. Milller
Washington, D.C.: NACA, 1928

Truax, T. R. [VerfasserIn]
291: Gluing practice at aircraft manufacturing plants and replair stations by T. R. Truax
Washington, D.C.: NACA, 1928

Heim, A. L. [VerfasserIn]
272: Special propeller protractor by A. L. Heim
Washington, D.C.: NACA, 1928

Havill, Clinton H. [VerfasserIn]
276: Helium tables by Clinton H. Havill
Washington, D.C.: NACA, 1928

Rhode, Richard V. [VerfasserIn]
277: Pressure distribution on wing ribs of the VE 7 and TS airplanes in flight 2 Pull ups by R. V. Rhode
Washington, D.C.: NACA, 1928

Zahm, A. F. [VerfasserIn]
278: An automatic speed sontrol for wind tunnels by A. F. Zahm
Washington, D.C.: NACA, 1928

Weick, Fred E. [VerfasserIn]
292: The drag of a J 5 radial air cooled engine by Fred E. Weick
Washington, D.C.: NACA, 1928

Weick, Fred E. [VerfasserIn]
301: Drag and cooling with various forms of cowling for a "whirlwind" engine in a cabin fuselage by Fred E. Weick
Washington, D.C.: NACA, 1928

Carroll, Thomas [VerfasserIn]; MacAvoy, William H. [VerfasserIn]
293: The formation of ice upon exposed parts of an airplane in flight by Thomas Carroll and William H. MacAvoy
Washington, D.C.: NACA, 1928

Weick, Fred E. [VerfasserIn]
271: Full scale drag tests on variuos parts of Sperry Messenger airplane by Fred E. Weick
Washington, D.C.: NACA, 1928

Carroll, Thomas [VerfasserIn]
273: The effect on performance of a cutaway center section by Thomas Carroll
Washington, D.C.: NACA, 1928

Weick, Fred E. [VerfasserIn]
274: The effect of the Sperry Messenger fuselage on the air flow at the propeller plane by Fred E. Weick
Washington, D.C.: NACA, 1928

Weick, Fred E. [VerfasserIn]
275: Determination of propeller deflection by means of static load tests on models by Fred E. Weick
Washington, D.C.: NACA, 1928

Carroll, Thomas [VerfasserIn]
287: A dangerous seaplane landing condition by Thomas Carroll
Washington, D.C.: NACA, 1928

Rawdon, Henry S. [VerfasserIn]
284: Corrosion embrittlement of duralumin 3 Effect of the previous treatment of sheet material on the susceptibility to this type of corrosion by Henry S. Rawdon
Washington, D.C.: NACA, 1928

Hicks, Chester W. [VerfasserIn]; Moore, Charles S. [VerfasserIn]
298: The determination of several spray characteristics of high speed oil engine injection system with an oscilloscope by Chester W. Hicks and Charles S. Moore
Washington, D.C.: NACA, 1928

Carroll, Thomas [VerfasserIn]; MacAvoy, William H. [VerfasserIn]
300: The variation in pressures in the cockpit of an airplane in flight by Thomas Carroll and William H. MacAvoy
Washington, D.C.: NACA, 1928

Rawdon, Henry S. [VerfasserIn]
283: Corrosion embrittlement of duralumin 2 Accelerated corrosion tests and the behavior of high-strength Aluminium alloys of different compositions by Henry S. Rawdon
Washington, D.C.: NACA, 1928

Wood, Donald H. [VerfasserIn]
280: Drag of exposed fittings and surface irregularities on airplane fuselages by Donald H. Wood
Washington, D.C.: NACA, 1928

Weick, Fred E. [VerfasserIn]
281: A comparison of propeller and centrifugal fans for circulating the air in a wind tunnel by Fred E. Weick
Washington, D.C.: NACA, 1928

Rawdon, Henry S. [VerfasserIn]
285: Corrosion embrittlement of duralumin 4 The use of protective coatings by Henry S. Rawdon
Washington, D.C.: NACA, 1928

Rawdon, Henry S. [VerfasserIn]
282: Corrosion embrittlement of duralumin 1 Practical aspects of the problem by Henry S. Rawdon
Washington, D.C.: NACA, 1928

Wagner, Herbert [VerfasserIn]
490: Structures of thin sheet metal their design and construction by Herbert Wagner
Washington, D.C.: NACA, 1928

Richardson, H. C. [VerfasserIn]
288: The reaction on a float bottom when making contact with water at high speeds by H. C. Richardson
Washington, D.C.: NACA, 1928

Trayer, G. W. [VerfasserIn]
296: Bearing strength of wood under steel aircraft bolts and washers and other factors influencing fitting design by G. W. Trayer
Washington, D.C.: NACA, 1928

Reid, Elliott G. [VerfasserIn]; Caroll, Thomas [VerfasserIn]
258: A warning concerting the take-off with heavy load by Elliott G. Reid and Thomas Carroll
Washington, D.C.: NACA, 1927

Weick, Fred E. [VerfasserIn]
260: Study of open jet wind tunnel cones by Fred Weick
Washington, D.C.: NACA, 1927

Henrickson, H. B. [VerfasserIn]
261: Tension experiments on diaphram metals by H. B. Henrickson
Washington, D.C.: NACA, 1927

Rizzo, Frank [VerfasserIn]
255: Precision of wing sections and consequent aerodynamic effects by Frank Rizzo
Washington, D.C.: NACA, 1927

Smith, Richard H. [VerfasserIn]
254: Method of correcting wind tunnel data for omitted parts of airplane models by R. H. Smith
Washington, D.C.: NACA, 1927

Hall, Donald A. [VerfasserIn]
257: Technical preparation of the airplane "Spirit of St. Louis" by Donald A. Hall
Washington, D.C.: NACA, 1927

Reid, Elliott G. [VerfasserIn]
266: Airfoil lift with changing angle of attack by Elliott G. Reid
Washington, D.C.: NACA, 1927

Dix, E. H. [VerfasserIn]
259: "Alclad" a new corroion resistant aluminium product by E. H. Dix
Washington, D.C.: NACA, 1927

Miller, Roy G. J. [VerfasserIn]
263: A load factor formula by Roy G. Miller
Washington, D.C.: NACA, 1927

Higgins, George J. [VerfasserIn]
264: Tests of the N.P.L. airship models in the variable density wind tunnel by George J. Higgins
Washington, D.C.: NACA, 1927

Green, M. W. [VerfasserIn]
265: Measurement of the moments of inertia of full scale airplanes by M. W. Green
Washington, D.C.: NACA, 1927

Mock, Richard M. [VerfasserIn]
269: The distribution of loads between the wings of a biplane having decalage by Richard M. Mock
Washington, D.C.: NACA, 1927

Weick, Fred E. [VerfasserIn]
235: Propeller design 1 Practical application of the blade element theory by Fred E. Weick
Washington, D.C.: NACA, 1926

Weick, Fred E. [VerfasserIn]
238: Propeller design 4 A simple method for determining the strength of propellers by Fred E. Weick
Washington, D.C.: NACA, 1926

Coleman, Donald G. [VerfasserIn]
233: NACA flight path angle and air speed recorder by Donald G. Coleman
Washington, D.C.: NACA, 1926

Weick, Fred E. [VerfasserIn]
236: Propeller design 2 Extension of test data on a familiy of model propellers by means of the modified blade element theory by Fred E. Weick
Washington, D.C.: NACA, 1926

Joachim, William F. [VerfasserIn]
234: An investigation of the characteristics of steel diaphragms for automatic fuel injection valves by W. F. Joachim
Washington, D.C.: NACA, 1926

Higgins, George J. [VerfasserIn]
243: The characteristics of the NACA M 12 airfoil section by George J. Higgins
Washington, D.C.: NACA, 1926

Shoemaker, James M. [VerfasserIn]
252: Resistance of a fifteen centimeter disk by James M. Shoemaker
Washington, D.C.: NACA, 1926

Weick, Fred E. [VerfasserIn]
237: Propeller design 3 A simple system based on model propeller test data by Fred E. Weick
Washington, D.C.: NACA, 1926

Joachim, William F. [VerfasserIn]; Case, Harold W. [VerfasserIn]
241: Tests of several bearing materials lubricated by gasoline by W. F. Joachim and Harold W. Case
Washington, D.C.: NACA, 1926

Jacobs, Eastman N. [VerfasserIn]
249: Effect of protruding gasoline tanks upton the characteristics of an airfoil by Eastman N. Jacobs
Washington, D.C.: NACA, 1926

Carroll, Thomas [VerfasserIn]; Mixon, R. E. [VerfasserIn]
251: The effect of tube length upon the recorded pressures from a pair of static orifices in a wing panel by T. Caroll and R. E. Mixon
Washington, D.C.: NACA, 1926

Munk, Max M. [VerfasserIn]
230: The spacing of orifices for the measurement of pressure distributions by Max M. Munk
Washington, D.C.: NACA, 1926

Bromley, Stevens [VerfasserIn]; Robinson, William H. [VerfasserIn]
232: The lateral failure of spars Stevens Bromley and William H. Robinson
Washington, D.C.: NACA, 1926

Higgins, George J. [VerfasserIn]
240: The NACA CYH airfoil section by George J. Higgins
Washington, D.C.: NACA, 1926

Castleman, R. A. [VerfasserIn]
231: The resistance to the steady motion of small spheres in fluids by R. A. Castleman
[Washington, D.C.]: NACA, 1926

Havill, Clinton H. [VerfasserIn]
248: The drag of airships 2 Drag of bare hulls by Clinton H. Havill
Washington, D.C.: NACA, 1926

Kemper, Carlton [VerfasserIn]
242: Improving the performance of a compression ignition engine by directing flow of the inlet air by Carlton Kemper
[Washington, D.C.]: NACA, 1926

Weick, Fred E. [VerfasserIn]
244: Navy propeller section characteristics as used in propeller design by Fred E. Weick
Washington, D.C.: NACA, 1926

Lesley, E. P. [VerfasserIn]
246: Test of a model propeller with symmetrical blade sections by E. P. Lesley
[Washington, D.C.]: NACA, 1926

Reid, J. E. [VerfasserIn]; Kirchner, Otto E. [VerfasserIn]
229: An altitude chamber for the study and calibration of aeronautical instruments by J. E. Reid and Otto E. Kirchner
Washington, D.C.: NACA, 1925

Ober, Shatswell [VerfasserIn]
214: Note on the Katzmayr effect on arifoill drag by Shatswell Ober
[Washington, D.C.]: NACA, 1925

Munk, Max M. [VerfasserIn]
221: Model tests on the economy and effectiveness of helicopter propellers by Max M. Munk
[Washington, D.C.]: NACA, 1925

Weick, Fred E. [VerfasserIn]
225: Propeller scale effect and body interference by Fred E. Weick
Washington, D.C.: NACA, 1925

Wilson, E. E. [VerfasserIn]
211: Aircraft engine design by E. E. Wilson
[Washington, D.C.]: NACA, 1925

Freeman, R. G. [VerfasserIn]
222: Air flow investigation for lacation of angle of attack head on a JN4h airplane by R. G. Freeman
[Washington, D.C.]: NACA, 1925

Warner, Edward P. [VerfasserIn]
226: Wind tunnel tests of fuselages and windshields by Edward P. Warner
Washington, D.C.: NACA, 1925

Warner, Edward P. [VerfasserIn]
215: The calculaltion of wing float displacement by Edward P. Warner
[Washington, D.C.]: NACA, 1925

Higgins, George J. [VerfasserIn]
219: The comparison of well-known and new wing sections tested in the variable density wind tunnel by George J. Higgins
[Washington, D.C.]: NACA, 1925

Rizzo, Frank [VerfasserIn]
228: The Flettner rotor ship in the light of the Kutta-Joukowski theory and of experimental results by Frank Rizzo
Washington, D.C.: NACA, 1925

Munk, Max M. [VerfasserIn]
216: The velocity distribution caused by an airplane at the points of a vertical plane containing the span by Max M. Munk
[Washington, D.C.]: NACA, 1925

Munk, Max M. [VerfasserIn]
217: Note on the air forces on a wing caused by pitching by Max M. Munk
[Washington, D.C.]: NACA, 1925

Weick, Fred E. [VerfasserIn]
212: Simplified propeller design for low powered airplanes by Fred E. Weick
[Washington, D.C.]: NACA, 1925

Matthews, Robertson [VerfasserIn]
213: Discharge characteristics of a high speed fuel injection engine by Robertson Matthews
[Washington, D.C.]: NACA, 1925

Warner, Edward P. [VerfasserIn]; Ober, Shatswell [VerfasserIn]
218: The estmation of airplane performance from wind tunnel tests on conventional airplane models by Edward P. Warner and Shatswell Ober
[Washington, D.C.]: NACA, 1925

Munk, Max M. [VerfasserIn]
227: Determination and classification of the aerodynamic properties of wing sections by Max M. Munk
Washington, D.C.: NACA, 1925

Lee, John G. [VerfasserIn]
208: Tests on duralumin columns for aircraft construction by John G. Lee
[Washington, D.C.]: NACA, 1924

Younger, John E. [VerfasserIn]
203: A short method of calculating torsional stresses in an airplane fuselage by John E. Younger
[Washington, D.C.]: NACA, 1924

Munk, Max M. [VerfasserIn]
197: Some tables of the factor of apparent additional mass by Max M. Munk
[Washington, D.C.]: NACA, 1924

Cronstedt, Val [VerfasserIn]
305: The logarithmic polar curve - its theory and application to the predetermination of airplane performance by Val Cronstedt
[Washington, D.C.]: NACA, 1924

Hall, Charles Ward [VerfasserIn]
206: Structural weight of aircraft as affected by the system of design by Charles Ward Hall
[Washington, D.C.]: NACA, 1924

Caldwell, F. W. [VerfasserIn]; Clay, N. S. [VerfasserIn]
201: Micarta propellers 4 Technical methods of design by F. W. Caldwell and N. S. Clay
[Washington, D.C.]: NACA, 1924

Munk, Max M. [VerfasserIn]
177: Note on the relative effect of the dihedral and the sweep back of airplane wings by Max M. Munk
[Washington, D.C.]: NACA, 1924

Munk, Max M. [VerfasserIn]
187: The induction factor used for computing the rolling moment due to the allerons by Max M. Munk
[Washington, D.C.]: NACA, 1924

Munk, Max M. [VerfasserIn]
192: Note on the pressure distribution over the hull of elongated airships with circular cross section by Max M. Munk
[Washington, D.C.]: NACA, 1924

Caldwell, F. W. [VerfasserIn]; Clay, N. S. [VerfasserIn]
198: Micarta propellers 1 Materials by F. W. Caldwell and N. S. Clay
[Washington, D.C.]: NACA, 1924

Matthews, Robertson [VerfasserIn]; Gardiner, Arthur W. [VerfasserIn]
180: Increasing the compression pressure in an engine by using a long intake pipe by Robertson Matthews and Arthur W. Gardiner
[Washington, D.C.]: NACA, 1924

Munk, Max M. [VerfasserIn]
190: Comparing the performance of geometrically similar airplanes by Max M. Munk
[Washington, D.C.]: NACA, 1924

Otey, N. S. [VerfasserIn]
189: Torsional strength of nickel steel and duralumin tubing as affected by the ratio of diameter to gage thickness by N. S. Otey
[Washington, DC]: NACA, 1924

Toussaint, A. [VerfasserIn]; Kerneis, .. [VerfasserIn]; Girault, .. [VerfasserIn]
202: Experimental investigation of the effect of an oscillating airstream (Katzmayr effect) on the characteristics of airfoils by Toussaint; Kerneis and Girault
[Washington, D.C.]: NACA, 1924

LePage, W. L. [VerfasserIn]; Nichols, J. T. [VerfasserIn]
191: The effect of wind tunnel turbulence upton the forces measured models by W. L. LePage and J. T. Nichols
[Washington, DC]: NACA, 1924

Diehl, Walter S. [VerfasserIn]
183: Static stability of seaplane floats and hulls by W. S. Diehl
[Washington, DC]: NACA, 1924

Munk, Max M. [VerfasserIn]
184: Note on vortices and on their relation to the lift of airfoils by Max M. Munk
[Washington, D.C.]: NACA, 1924

Caldwell, F. W. [VerfasserIn]; Clay, N. S. [VerfasserIn]
199: Micarta propellers 2 Method of construction by F. W. Caldwell and N. S. Clay
[Washington, D.C.]: NACA, 1924

Caldwell, F. W. [VerfasserIn]; Clay, N. S. [VerfasserIn]
200: Micarta propellers 3 General description of the design by F. W. Caldwell and N. S. Clay
[Washington, D.C.]: NACA, 1924

Burgess, C. P. [VerfasserIn]
194: A method of determining the dimensions and horsepower of an airship for any given performance by C. P. Burgess
[Washington, D.C.]: NACA, 1924

Munk, Max M. [VerfasserIn]
195: On the distribution of lift along the span of an airfoil with displaced ailerons by Max M. Munk
[Washington, D.C.]: NACA, 1924

Munk, Max M. [VerfasserIn]
196: Remarks on the pressure distribution over the surface of an ellipsoid, moving translationally through a perfect fluid by Max M. Munk
[Washington, D.C.]: NACA, 1924

Reid, Elliott G. [VerfasserIn]
209: Tests of rotating cylinders by Elliot G. Reid
[Washington, D.C.]: NACA, 1924

DuBois, R. N. [VerfasserIn]
210: The testing of aviation engines under approximate altitude conditions by R. N. DuBois
[Washington, D.C.]: NACA, 1924

Munk, Max M. [VerfasserIn]
207: The simplifying assumptions, reducing the strict application of classical hydrodynamics to practical aeronautical computations paper read at International Congress for Applied Mechanics, Delft, Holland, April 22 - 28, 1934 by Max M. Munk
Washington, D.C.: NACA, 1924

King, Paul B. [VerfasserIn]; Carroll, Thomas [VerfasserIn]
193: High altitude flying by Paul B. King and Thomas Carroll
[Washington, D.C.]: NACA, 1924

Rizzo, Frank [VerfasserIn]
204: A study of static stability of airships by Frank Rizzo
Washington, D.C.: NACA, 1924

Reid, H. J. E. [VerfasserIn]
150: Notes o the N.A.C.A. control force recorder by H. J. E. Reid
[Washington, DC]: NACA, 1923

Reid, H. J. E. [VerfasserIn]
156: The NACA recording tachometer and angle of attack recorder by H. J. E. Reid
[Washington, DC]: NACA, 1923

Schwamb, T. A. [VerfasserIn]; Smith, C. S. [VerfasserIn]
151: Tests on built-up airplane struts having initial tension in outside fibers by T. A. Schwamb and C. S. Smith
[Washington, DC]: NACA, 1923

Rettew, H. F. [VerfasserIn]; Thumin, C. [VerfasserIn]
165: Tests on riveted joints in sheet duralumin by H. F. Rettew and C. Thumin
[Washington, DC]: NACA, 1923

Warner, John A. C. [VerfasserIn]
123: An optical altitude indicator for night landing by John A. C. Warner
[Washington, DC]: NACA, 1923

Shoemaker, James M. [VerfasserIn]; Lee, John G. [VerfasserIn]
161: Preliminary study of the damping factor in roll by James M. Shoemaker and John G. Lee
[Washington, D.C.]: NACA, 1923

Diehl, Walter S. [VerfasserIn]
144: Notes on the design of ailerons by W. S. Diehl
[Washington, DC]: NACA, 1923

Matthews, Robertson [VerfasserIn]
149: Influences in the selection of a cycle for small high speed engines running on solid or airless injection with compression ignition by Robertson Matthews
[Washington, D.C.]: NACA, 1923

Ronan, K. M. [VerfasserIn]
154: An instrument for recording the position of airplane control surfaces by K. M. Ronan
[Washington, DC]: NACA, 1923

Joachim, William F. [VerfasserIn]
157: An impulse electric motor for driving recording instruments by W. F. Joachim
[Washington, DC]: NACA, 1923

Matthews, Robertson [VerfasserIn]; Gardiner, Arthur W. [VerfasserIn]
159: The time lag and interval of discharge with a spring actuated fuel injection pump by Robertson Matthews and Arthur W. Gardiner
[Washington, D.C.]: NACA, 1923

Warner, Edward P. [VerfasserIn]
167: Wind tunnel tests of five strut sections in yaw by Edward P. Warner
[Washington, D.C.]: NACA, 1923

Ford, James B. [VerfasserIn]
172: The Nichols wing cutting equipment by James B. Ford
[Washington, D.C.]: NACA, 1923

Ware, Marsden [VerfasserIn]
40: Effect of the reversal of air flow upon the discharge coefficient of Durley orifices by Marsden Ware
[Washington, D.C.]: NACA, 1921

Diehl, Walter S. [VerfasserIn]
42: The determination of downwash by Walter S. Diehl
[Washington, DC]: NACA, 1921

Norton, F. H. [VerfasserIn]; Bacon, D. L. [VerfasserIn]
36: N.A.S.A. langley field wind tunnel apparatus the tilting manometer by F. H. Norton and D. L. Bacon
[Washington, D.C.]: NACA, 1921

Silsbee, Francis B. [VerfasserIn]
32: Causes of cracking of ignition cable by F. B. Silsbee
[Washington, D.C.]: NACA, 1921

Davidson, W. E. [VerfasserIn]; Bacon, D. L. [VerfasserIn]
37: The determinaton of the effective resistance of a spindle supporting a model aerofoil by W. E. Davidson and D. L. Bacon
[Washington, D.C.]: NACA, 1921

Norton, F. H. [VerfasserIn]
54: The factors that determine the minimum speed of an airplane by F. H. Norton
[Washington, D.C.]: NACA, 1921

Riabouchinsky, Dimitri Pavlovitch [VerfasserIn]
44: On the resistance of spheres and ellipsoids in wind tunnels by D. P. Riabouchinsky
[Washington, DC]: NACA, 1921

Heidelberg, Ing. von [VerfasserIn]
38: Measurements of rudder moments on an airplane during flight by Ing. v. Heidelberg
[Washington, D.C.]: NACA, 1921

Sparrow, Stanwood W. [VerfasserIn]
55: Airplane crashes: Engine troubles a possible explanation by Stanwood W. Sparrow
Washington, D.C.: NACA, 1921

Riabouchinsky, Dimitri Pavlovitch [VerfasserIn]
49: On the resistance of the air at high speeds and on the automatic rotation of projectiles by D. Riabouchinski
[Washington, D.C.]: NACA, 1921

Wieselsberger, Carl [VerfasserIn]
33: The effect of the nature of surfaces on resistance, as tested on struts by C. Wieselsberger
[Washington, D.C.]: NACA, 1921

Toussaint, A. [VerfasserIn]
43: Note on the resistance of polished cylinders (and cylindrical wires) with generatrices perpendicular to the airstream by A. Toussaint
[Washington, D.C.]: NACA, 1921

Devillers, René [VerfasserIn]
11: The problem of the turbo-compressor extract from "The Internal Combustion Engine" by René Devillers
Washington, D.C.: NACA, 1920

Norton, F. H. [VerfasserIn]
22: The photographic recording of small motions by F. H. Norton
[Washington, D.C.]: NACA, 1920

Zahm, A. F. [VerfasserIn]
23: Horizontal buoyancy in wind tunnel by A. F. Zahn
[Washington, D.C.]: NACA, 1920

Margoulis, W. [VerfasserIn]
19: The steadiness factor in engine sets by W. Margoulis
Washington, D.C.: NACA, 1920

Knight, William [VerfasserIn]
17: Italian and French experiments on wind tunnels by Wm. Knight
Washington, D.C.: NACA, 1920

Idrac, Pierre [VerfasserIn]
13: Soaring flight in Guinea by P. Idrac
Washington, D.C.: NACA, 1920

Sparrow, Stanwood W. [VerfasserIn]
39: High thermal efficiency in airplane service by S. W. Sparrow
[Washington, D.C.]: NACA, 1920

Baumann, Alexander [VerfasserIn]
29: Progress made in the construction of giant airplanes in germany during the war by A. Baumann
[Washington, D.C.]: NACA, 1920

Margoulis, W. [VerfasserIn]
20: Notes on specifications for french airplane competitions by W. Margoulis
Washington, D.C.: NACA, 1920

Sparrow, Stanwood W. [VerfasserIn]
14: Increase in maximum pressures produced by preignition in internal combustion engines by S. W. Sparrow
[Washington, D.C.]: NACA, 1920

Norton, F. H. [VerfasserIn]
30: Design of recording wind tunnel balances by S. W. Sparrow
[Washington, D.C.]: NACA, 1920

Toussaint, A. [VerfasserIn]
21: Drag or negative traction of geared down supporting propellers in the downward vertical gilde of a helicopter by A. Toussaint
[Washington, D.C.]: NACA, 1920

Wood, K. D. [VerfasserIn]
26: A variable speed fan dynamometer by Karl D. Wood
[Washington, D.C.]: NACA, 1920