> Verlagsreihe
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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
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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
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Airfoil section characteristics at high angles of attack by Laurence K. Loftin
Washington, DC: National Advisory Committee for Aeronautics, 1954
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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
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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
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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
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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
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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
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Landing-gear impact by W. Flügge
Washington, DC: National Advisory Committee for Aeronautics, 1952
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High-speed subsonic characteristics of 16 NACA 6-series airfoil sections by Milton D. Van Dyke
Washington, DC: National Advisory Committee for Aeronautics, 1952
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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
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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
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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
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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
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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]
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Principles, practice, and progress of noise reduction in airplanes by Albert London
Washington, DC: NACA, 1940
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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
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A simple method of obtaining span load distributions by Albert Sherman
Washington, D.C.: NACA, 1939
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Corrugated metal diaphragms for aircraft pressure measuring instruments by W. A. Wildhack and V. H. Goerke
Washington, D.C.: NACA, 1939
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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
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Theory of automatic control of airplanes by Herbert K. Weiss
Washington, DC: NACA, 1939
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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]
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Tests of a gust alleviating flap in [...] by Philip Donely and C. C. Shufflebarger
Washington, D.C.: NACA, 1939
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Some fundamental considerations in regard to the use of power in landing an airplane by Walter S. Diehl
[Washington, DC]: NACA, [1939]
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The effects of surface waviness and of rib stitching on wing drag by Manley J. Hood
[Washington, DC]: NACA, [1939]
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The effects of some common surface irregula[rities] on wing drag by Manley J. Hood
[Washington, DC]: NACA, [1939]
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Wind tunnel investigation of ground effect on wings with flaps by Isidore G. Recant
Washington, D.C.: NACA, 1939
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A comparison of several tapered wings designed to avoid tip stalling by Raymond F. Anderson
[Washington, DC]: NACA, [1939]
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A method of estimating the critical buckling load for structural members by Eugene E. Lundquist
[Washington, DC]: NACA, [1939]
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Local instability of centrality loaded columns of channel section and Z-section by Eugene E. Lundquist
[Washington, DC]: NACA, [1939]
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Adhesion of ice in its relation to the de-icing of airplanes by A. M. Rothrock and R. F. Selden
[Washington, DC]: NACA, [1939]
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An approximate spin design criterion for monoplanes by Oscar Seidman and Charles J. Donlan
[Washington, DC]: NACA, [1939]
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Combined beam column stresses of aluminium alloy channel sections by R. Gottlieb, T. M. Thompson and E. C. Witt
[Washington, DC]: NACA, [1939]
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Flight tests of retractable ailerons on a highly tapered wing by J. W. Wetmore
[Washington, DC]: NACA, [1939]
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Compressive tests of a monocoque box by Walter Ramberg, Albert E. McPherson, and Sam Levy
[Washington, DC]: NACA, [1939]
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Photoelastic analysis of three-dimensional stress systems using scattered light by R. Weller and J. K. Bussey
[Washington, DC]: NACA, [1939]
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Operational treatment of the nonuniform-lift theory in airplane dynamics by Robert T. Jones
Washington, DC: NACA, 1938
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Physical properties of synthetic res[ins] by Meyer Fishbein
[Washington, DC]: NACA, [1938]
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The effect of air passage length on the optimum fin spacing for maximum cooling by Maurice J. Brevoort
Washington, DC: NACA, 1938
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Generalized analysis of experimental observations in problems of elastic stability by Eugene E. Lundquist
[Washington, DC]: NACA, [1938]
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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]
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Some aspects of the stalling of modern low wing monoplanes by Hartley A. Soulé and Melvin N. Gough
[Washington, DC]: NACA, [1938]
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Résumé of air load data on slats and flaps by Carl J. Wenzinger and Francis M. Rogallo
[Washington, DC]: NACA, [1938]
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A study of flying boat take-off by Walter S. Diehl
[Washington, DC]: NACA, [1938]
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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]
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Fatigue testing of wing beams by the resonance method by William M. Bleakney
[Washington, DC]: NACA, [1938]
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Circulation measurements about the tip of an airfoil during flight through a gust by Arnold M. Kuethe
[Washington, DC]: NACA, [1938]
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The unsteady lift of a finite wing by Robert T. Jones
[Washington, DC]: NACA, [1938]
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Torsional stability of aluminium alloy seamless tubing by R. L. Moore and D. A. Paul
[Washington, DC]: NACA, [1938]
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The estimation of the rate of change of yawing moment with sideslip by Frederick H. Imlay
[Washington, DC]: NACA, [1938]
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A method of rapidly estimating the position of the laminar separation point by Albert E. von Doenhoff
[Washington, DC]: NACA, [1938]
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Tests of a contra-propeller for aircraft by William M. Benson
Washington, DC: NACA, 1938
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Theoretical span loading and moments of tapered wings produced by aileron deflection by H. A. Pearson
Washington, D.C.: NACA, 1937
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Plastics as structural materials [...] by G. M. Kline
[Washington, DC]: NACA, [1937]
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Tandem air propellers by E. P. Lesley
[Washington, D.C.]: NACA, [1937]
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Wind tunnel tests of a Clark Y wing with "Maxwell" leading edge slots by William E. Gauvain
[Washington, DC]: NACA, [1937]
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Stability of structural members under axial load by Eugene E. Lundquist
[Washington, DC]: NACA, [1937]
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Notes on the calculation of the minimum horizontal tail surface for airplanes equipped with wing flaps by Hartley A. Soulé
[Washington, DC]: NACA, [1937]
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Maximum forces applied by pilots to wheel type controls by William H. McAvoy
[Washington, DC]: NACA, [1937]
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Pressure distribution over a Clark Y-H airfoil section with a split flap by Carl J. Wenzinger
[Washington, DC]: NACA, [1937]
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Wind tunnel tests of a Clark Y wing having split flaps with gaps by Carl J. Wenzinger
[Washington, DC]: NACA, [1937]
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The measurement of air speed of airplanes by F. L. Thompson
[Washington, DC]: NACA, [1937]
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Calculations of the effect of wing twist on the air forces acting on a monoplane wing by G. Dätwyler
[Washington, DC]: NACA, [1937?]
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The reduction of aileron operating force by differential linkage by Robert T. Jones and Albert I. Nerken
Washington, D.C.: NACA, 1936
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Remarks on the elastic axis of shell wings by Paul Kuhn
Washington, D.C.: NACA, 1936
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Effect of changes in tail arrangement upon the spinning of a low wing monoplane [model] by C. H. Zimmerman
[Washington, DC]: NACA, [1936]
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Tank tests of a model of the NC flying boat hull - NACA model 44 by Joe W. Bell
[Washington, DC]: NACA, [1936]
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The frequencies of cantilever wings in beam and torsional vibration by C. P. Burgess
Washington, D.C.: NACA, 1936
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Considerations of the take-off problem by Edwin P. Hartman
[Washington, DC]: NACA, [1936]
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Piloting technique for recovery from spins by W. H. McAvoy
[Washington, DC]: NACA, [1936]
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Notes on the technique of landing airplanes equipped with wing flaps by Melvin N. Gough
[Washington, DC]: NACA, [1936]
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Full scale force and pressure distribution tests on a tapered U.S.A. 45 airfoil by John F. Parsons
Washington, D.C.: NACA, 1935
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Strength tests of thin walled duralumin cylinders in combined transverse shear and bending by Eugene E. Lundquist
Washington, D.C.: NACA, 1935
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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
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Aerodynamic characteristics of several airfoils of low aspect ratio by C. H. Zimmerman
[Washington, DC]: NACA, [1935]
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The initial torsional stiffness of shells with interior webs by Paul Kuhn
[Washington]: NACA, [1935]
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Bending stresses due to torsion in cantile[ver box beams] by Paul Kuhn
[Washington]: NACA, [1935]
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Strength tests of thin walled duralumin cylinders of elliptic section by Eugene E. Lundquist and Walter F. Burke
Washington, D.C.: NACA, 1935
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Development of the NACA slot lip [aileron] by Fred E. Weick and Joseph [A. Shortal]
[Washington, DC]: NACA, [1935]
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Wind tunnel tests of wing flaps suitable for direct control of glide-fath angle by Fred E. Weick
[Washington, DC]: NACA, [1935]
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The compressibility burble by John Stack
[Washington, DC]: NACA, [1935]
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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]
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A study of factors affecting the steady spin of an airplane by Nathan F. Scudder
[Washington, DC]: NACA, [1935]
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Calculated effect of various types of flap on take-off over obstacles by J. W. Wetmore
[Washington, DC]: NACA, [1935]
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Flight tests of a balanced split flap with particular reference to rapid operation by H. A. Soule
[Washington, DC]: NACA, [1935]
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A study of the pitching moments and the stability characteristics of monoplanes by George J. Higgins
Washington, D.C.: NACA, 1934
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The wave suppressors used in the N.A.C.A. tank by Starr Truscott
Washington, D.C.: NACA, 1934
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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
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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
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Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model by J. M. Bamber
Washington, D.C.: NACA, 1934
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Measurement of altitude in blind flying by W. G. Brombacher
Washington, D.C.: NACA, 1934
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Wind tunnel tests of a wing with a trailing edge auxiliary airfoil used as a flap by Richard W. Noyes
[Washington, DC]: NACA, [1934]
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The torsional stiffness of thin duralumin shells subjected to large torques by Paul Kuhn
Washington, D.C.: NACA, 1934
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Aerodynamic investigation of a cup anemometer by John D. Hubbard and George P. Brescoll
Washington, D.C.: NACA, 1934
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Experimental verification of Theodorsen's theoretical jet boundary correction factors by George Van Schliestett
Washington, D.C.: NACA, 1934
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Effect of the surface condition of a wing on the aerodynamic characteristics of an airplane by S. J. DeFrance
[Washington, DC]: NACA, [1934]
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Landing characteristics of an autogiro by William C. Peck
[Washington, DC]: NACA, [1934]
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Effect of retractable spoiler location on rolling and yawing moment coefficients by J. A. Shortal
[Washington, DC]: NACA, [1934]
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Landing shock recorder by Maurice J. Brevoort
[Washington, DC]: NACA, 1934
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A method of calculating the performance of controllable propellers, with sample computations by Edwin P. Hartman
Washington, D.C.: NACA, 1934
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Wind tunnel measurements of air loads on split flaps by Carl J. Wenzinger
Washington, D.C.: NACA, 1934
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Thank tests of flat and V bottom planing surfaces by James M. Shoemaker
Washington, D.C.: NACA, 1934
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Full scale drag tests of landing lamps by C. H. Dearborn
Washington, D.C.: NACA, 1934
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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
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Engine performance with a hydrogenated safety fuel by Oscar W. Schey and Alfred W. Young
Washington, D.C.: NACA, 1933
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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]
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Simplified aerodynamic analysis of the cyclogiro rotating wing sys[tem] by John B. Wheatley
[Washington, DC]: NACA, [1933]
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Wind tunnel tests of a cyclogiro rotor by John B. Wheatley and Ray Windler
[Washington, DC]: NACA, [1933]
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Strength test of thin walled duralu[min cylinders] in pure bending by Eugene E. Lundquist
[Washington, DC]: NACA, [1933]
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The drag of streamline wires by Eastman N. Jacobs
[Washington, DC]: NACA, [1933]
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The reduction in drag of a forward sloping windshield by Eastman N. Jacobs
[Washington, DC]: NACA, [1933]
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The effect of split trailing edge wing flaps on the aerodynamic characteristics of a parasol monoplane by Rudolf N. Wallace
[Washington, DC]: NACA, [1933]
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Effect of aileron displacement on wing characteristics by R. H. Heald
Washington, D.C.: NACA, 1933
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The importance of auto ignition lag in knocking by E. S. Taylor
Washington, D.C.: NACA, 1933
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Experiments with a counter propeller by E. P. Lesley
Washington, D.C.: NACA, 1933
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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
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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
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Charts for determining the pitching moment of tapered wings with sweepback and twist by Raymond F. Anderson
Washington, D.C.: NACA, 1933
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Jet propulsion with special reference to thrust augmentors by G. B. Schubauer
Washington, D.C.: NACA, 1933
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Mercerization of cotton for strength with special reference to aircraft cloth by J. B. Wilkie
Washington, D.C.: NACA, 1933
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Effect of stabilizer [...] by M. J. Bamber
[Washington, D.C.]: NACA, [ca. 1933]
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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
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Estimation of the variation of thrust horsepower with air speed by Shatswell Ober
Washington, D.C.: NACA, 1933
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The aerodynamic effect of a retractable landing gear by Smith J. DeFrance
Washington, D.C.: NACA, 1933
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The aerodynamic characteristics of airfoils as affected by surface roughness by Ray W. Hocker
Washington, D.C.: NACA, 1933
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Some characteristics of sprays obtained from pintle type injection nozzles by E. T. Marsh and C. D. Waldron
Washington, D.C.: NACA, 1933
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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
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Valve timing of engines having intake pressures higher than exhaust by Edward S. Taylor
Washington, D.C.: NACA, 1932
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The effect of propellers and nacelles on the landing speeds of tractor monoplanes by Ray Windler
Washington, D.C.: NACA, 1932
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Wind tunnel tests of a hall high lift wing by Fred E. Weick and Robert Sanders
Washington, D.C.: NACA, 1932
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Preliminary photomicrographic studies of fuel sprays by Dana W. Lee and Robert C. Spencer
Washington, D.C.: NACA, 1932
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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
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The compressive strength of duralumin columns of equal angle section by Eugene E. Lundquist
Washington, D.C.: NACA, 1932
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The aerodynamic characteristics of airfoils at negative angles of attack by Raymond F. Anderson
Washington, D.C.: NACA, 1932
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Characteristics of an airfoil as affected by fabric sag by Kenneth E. Ward
[Washington, DC]: NACA, [1932]
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Methods of visually determining the air flow around airplanes by Melvin N. Gough and Ernest Johnson
[Washington, DC]: NACA, [1932]
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Preliminary tests on the vaporization of fuel sprays by A. M. Rothrock
Washington, D.C.: NACA, 1932
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Experiments on the distribution of fuel in fuel sprays by Dana W. Lee
Washington, D.C.: NACA, 1932
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Strength tests on thin walled duralumin cylinders in torsion by Eugene E. Lundquist
Washington, D.C.: NACA, 1932
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Effect of engine operating conditions on the vaporization of safety fuels by A. M. Rothrock and C. D. Waldron
Washington, D.C.: NACA, 1932
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Drag tests of 4 9 scale model engine nacelles with various cowlings by Ray Windler
Washington, D.C.: NACA, 1932
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Influence of several factors on ignition lag in a compression ignition engine by Harild C. Gerrish and Fred Voss
Washington, D.C.: NACA, 1932
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The pressure distribution over a long elliptical wing tip on a biplane in flight by Richard V. Rhode
Washington, D.C.: NACA, 1932
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Compression ignition engine tests of several fuels by J. A. Spanogle
Washington, D.C.: NACA, 1932
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Meteorological conditions during the formation of ice on aircraft by L. T. Samuels
Washington, D.C.: NACA, 1932
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Wind tunnel tests of the fowler variable area wing by Fred E. Weick and Robert C. Platt
Washington, D.C.: NACA, 1932
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The gaseous explosive reaction at constant pressure - further data on the effect of inert gases by F. W. Stevens
Washington, D.C.: NACA, 1932
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Working charts for the stress analysis [of elliptic rings] by Walter F. Burke
[Washington, DC]: NACA, 1932
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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
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An integrating manometer for use in wind tunnel pressure distribution measurements by Richard W. Noyes
Washington, D.C.: NACA, 1931
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Effect of high air velocities on the distribution and penetration of a fuel spray by A. M. Rothrock
Washington, D.C.: NACA, 1931
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An investigation of cotton for parachute cloth by Wm. D. Appel and R. K. Worner
Washington, D.C.: NACA, 1931
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The prevention of ice formation on gasoline tank vents by Theodore Theodorsen and William C. Clay
Washington, D.C.: NACA, 1931
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Penetration and duration of fuel sprays from pump injection system by A. M. Rothrock and E. T. Marsh
Washington, D.C.: NACA, 1931
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Some characteristics of fuel sprays at low injection pressures by A. M. Rothrock and C. D. Waldron
Washington, D.C.: NACA, 1931
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The interference effects on an airfoil of a flat plate at mid span position by Kenneth E. Ward
Washington, D.C.: NACA, 1931
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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]
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The effect of injection valve opening pressure on spray tip penetration by A. M. Rothrock and E. T. Marsh
Washington, D.C.: NACA, 1931
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Metal truss wing spars by Andrew E. Swickard
Washington, D.C.: NACA, 1931
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Comparison of weights of 17ST and steel tubular structural members used in aircraft construction by E. C. Hartmann
Washington, D.C.: NACA, 1931
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A suggested method for measuring turbulence by C. Fayette Taylor
Washington, D.C.: NACA, 1931
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Basic requirements of fuel injection nozzles for quiescent combustion chambers by J. A. Spanogle and H. H. Foster
Washington, D.C.: NACA, 1931
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Characteristics of two sharp nosed airfoils having reduced spinning tendencies by Eastman N. Jacobs
[Washington, DC]: NACA, [1931]
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The effect of small variations in profile of airfoils by Kenneth E. Ward
Washington, D.C.: NACA, 1931
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Lift and drag characteristics of a cabin monoplane determined in flight by F. L. Thompson and P. H. Keister
Washington, D.C.: NACA, 1931
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The behavior of conventional airplanes in situations thought to lead to most crashes by Fred E. Weick
Washington, D.C.: NACA, 1931
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Interference effects and drag of struts on a monoplane wing by Kenneth E. Ward
Washington, D.C.: NACA, 1931
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Torsion in box wings by John B. Wheatley
Washington, D.C.: NACA, 1931
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The variation in pressure in the cabin of an airplane in flight by Melvin N. Gough
Washington, D.C.: NACA, 1931
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Moments of inertia of airplanes by Marvel P. Miller and Hartley A. Soulé
Washington, D.C.: NACA, 1931
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Tests of six symmetrical airfoils in the variable density wind tunnel by Easrman N. Jacobs
Washington, D.C.: NACA, 1931
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Effect of nose shape on characteristics of symmetrical airfoils by Robert M. Pinkerton
Washington, D.C.: NACA, 1931
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A method for reducing the temperature of exhaust manifolds by Oscar W. Schey and Alfred W. Young
Washington, D.C.: NACA, 1931
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Alterations and tests of the "Farnboro" engine indicator by John H. Collins
Washington, D.C.: NACA, 1930
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An investigation of airplane landing speeds by Kenneth F. Ridley
Washington, D.C.: NACA, 1930
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An accurate method of measuring the moments of inertia of airplanes by M. P. Miller
Washington, D.C.: NACA, 1930
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Bending tests of metal monocoque fuselage construction by Ralph W. Mossman and Russell G. Robinson
Washington, D.C.: NACA, 1930
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Effect of orifice length diameter ratio on spray characteristics by A. G. Gelalles
Washington, D.C.: NACA, 1930
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Analytical determination of the load on a trailing dege flap by Robert M. Pinkerton
Washington, D.C.: NACA, 1930
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Some characteristics of fuel sprays from open nozzles by A. M. Rothrock and D. W. Lee
Washington, D.C.: NACA, 1930
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Identification of aircraft tubing by rockwell test by Horace Knerr
Washington, D.C.: NACA, 1930
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Some effects of air and fuel oil temperatures on spray penetration and dispersion by A. G. Gelalles
Washington, D.C.: NACA, 1930
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Pressure distribution on the tail surfaces of a PW-9 pursuit airplane in flight by Richard V. Rhode
Washington, D.C.: NACA, 1930
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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
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Injection lags in a common rail fuel injection system by A. M. Rothrock
Washington, D.C.: NACA, 1930
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Test of an adjustable pitch model propeller at four blade settings by E. P. Lesley
Washington, D.C.: NACA, 1930
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The structure and properties of parachute cloths by H. J. McNicholas and A. F. Hedrick
Washington, D.C.: NACA, 1930
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The prevention of the ice hazard on airplanes by William C. Geer and Merit Scott
Washington, D.C.: NACA, 1930
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The formation of ice upon airplanes in flight by Thomas Carroll and William H. MacAvoy
Washington, D.C.: NACA, 1929
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Condensed data on the aircraft engines of the world compiled by C. S. Fliedner
Washington, D.C.: NACA, 1929
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Some studies on the aerodynamic effect of the gap between airplane wings and fuselages by Shatswell Ober
Washington, D.C.: NACA, 1929
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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
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A new method for the prediction of airplane performance by E. P. Lesley and E. G. Reid
Washington, D.C.: NACA, 1929
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Corrosion embrittlement of duralumin 5 The results of weather exposure tests by Henry S. Rawdon
Washington, D.C.: NACA, 1929
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Curves showing column strength of steel and duralumin tubing by Orrin E. Ross
Washington, D.C.: NACA, 1929
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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
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Spiral tendency in blind flying by Thomas Carroll and William H. MacAvoy
Washington, D.C.: NACA, 1929
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Viscosity of diesel engine fuel oil under pressure by Mayo D. Hersey
Washington, D.C.: NACA, 1929
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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
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Tests of four racing type airfoils in the twenty-foot propeller research tunnel by Fred E. Weick
Washington, D.C.: NACA, 1929
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Some experiments on autorotation of an airfoil by Shatswell Ober
Washington, D.C.: NACA, 1929
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The drag and interference of a nacelle in the presence of a wing by Eastman N. Jacobs
Washington, D.C.: NACA, 1929
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Wind tunnel pressure distribution tests on an airfoil with trailling edge flap by Carl J. Wenzinger and Oscar Loeser
Washington, D.C.: NACA, 1929
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The impact on seaplane floats during landing by Th. von Karman
Washington, D.C.: NACA, 1929
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Full scale investigation of the drag of a wing radiator by Fred E. Weick
Washington, D.C.: NACA, 1929
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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
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The variation in pressures in the cockpit of an airplane in flight by Thomas Carroll and William H. MacAvoy
Washington, D.C.: NACA, 1928
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Resistance of streamline wires by George L. DeFoe
Washington, D.C.: NACA, 1928
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Drag of exposed fittings and surface irregularities on airplane fuselages by Donald H. Wood
Washington, D.C.: NACA, 1928
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A comparison of propeller and centrifugal fans for circulating the air in a wind tunnel by Fred E. Weick
Washington, D.C.: NACA, 1928
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Corrosion embrittlement of duralumin 4 The use of protective coatings by Henry S. Rawdon
Washington, D.C.: NACA, 1928
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A dangerous seaplane landing condition by Thomas Carroll
Washington, D.C.: NACA, 1928
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Preliminary biplane tests in the variable density wind tunnel by James M. Shoemaker
Washington, D.C.: NACA, 1928
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The reaction on a float bottom when making contact with water at high speeds by H. C. Richardson
Washington, D.C.: NACA, 1928
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Welding of high chromium steels by W. B. Milller
Washington, D.C.: NACA, 1928
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Gluing practice at aircraft manufacturing plants and replair stations by T. R. Truax
Washington, D.C.: NACA, 1928
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Corrosion embrittlement of duralumin 1 Practical aspects of the problem by Henry S. Rawdon
Washington, D.C.: NACA, 1928
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Research on the control of airplanes by B. Melvill Jones
Washington, D.C.: NACA, 1928
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Structures of thin sheet metal their design and construction by Herbert Wagner
Washington, D.C.: NACA, 1928
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The formation of ice upon exposed parts of an airplane in flight by Thomas Carroll and William H. MacAvoy
Washington, D.C.: NACA, 1928
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Full scale drag tests on variuos parts of Sperry Messenger airplane by Fred E. Weick
Washington, D.C.: NACA, 1928
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Special propeller protractor by A. L. Heim
Washington, D.C.: NACA, 1928
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The effect on performance of a cutaway center section by Thomas Carroll
Washington, D.C.: NACA, 1928
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The effect of the Sperry Messenger fuselage on the air flow at the propeller plane by Fred E. Weick
Washington, D.C.: NACA, 1928
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Determination of propeller deflection by means of static load tests on models by Fred E. Weick
Washington, D.C.: NACA, 1928
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Helium tables by Clinton H. Havill
Washington, D.C.: NACA, 1928
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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
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An automatic speed sontrol for wind tunnels by A. F. Zahm
Washington, D.C.: NACA, 1928
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The drag of a J 5 radial air cooled engine by Fred E. Weick
Washington, D.C.: NACA, 1928
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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
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Method of correcting wind tunnel data for omitted parts of airplane models by R. H. Smith
Washington, D.C.: NACA, 1927
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Precision of wing sections and consequent aerodynamic effects by Frank Rizzo
Washington, D.C.: NACA, 1927
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Technical preparation of the airplane "Spirit of St. Louis" by Donald A. Hall
Washington, D.C.: NACA, 1927
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A warning concerting the take-off with heavy load by Elliott G. Reid and Thomas Carroll
Washington, D.C.: NACA, 1927
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"Alclad" a new corroion resistant aluminium product by E. H. Dix
Washington, D.C.: NACA, 1927
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Study of open jet wind tunnel cones by Fred Weick
Washington, D.C.: NACA, 1927
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Tension experiments on diaphram metals by H. B. Henrickson
Washington, D.C.: NACA, 1927
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A load factor formula by Roy G. Miller
Washington, D.C.: NACA, 1927
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Tests of the N.P.L. airship models in the variable density wind tunnel by George J. Higgins
Washington, D.C.: NACA, 1927
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Measurement of the moments of inertia of full scale airplanes by M. W. Green
Washington, D.C.: NACA, 1927
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Airfoil lift with changing angle of attack by Elliott G. Reid
Washington, D.C.: NACA, 1927
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The distribution of loads between the wings of a biplane having decalage by Richard M. Mock
Washington, D.C.: NACA, 1927
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Improving the performance of a compression ignition engine by directing flow of the inlet air by Carlton Kemper
[Washington, D.C.]: NACA, 1926
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The spacing of orifices for the measurement of pressure distributions by Max M. Munk
Washington, D.C.: NACA, 1926
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Navy propeller section characteristics as used in propeller design by Fred E. Weick
Washington, D.C.: NACA, 1926
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The drag of airships 2 Drag of bare hulls by Clinton H. Havill
Washington, D.C.: NACA, 1926
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The resistance to the steady motion of small spheres in fluids by R. A. Castleman
[Washington, D.C.]: NACA, 1926
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Test of a model propeller with symmetrical blade sections by E. P. Lesley
[Washington, D.C.]: NACA, 1926
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The lateral failure of spars Stevens Bromley and William H. Robinson
Washington, D.C.: NACA, 1926
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Propeller design 1 Practical application of the blade element theory by Fred E. Weick
Washington, D.C.: NACA, 1926
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Propeller design 4 A simple method for determining the strength of propellers by Fred E. Weick
Washington, D.C.: NACA, 1926
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The NACA CYH airfoil section by George J. Higgins
Washington, D.C.: NACA, 1926
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NACA flight path angle and air speed recorder by Donald G. Coleman
Washington, D.C.: NACA, 1926
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An investigation of the characteristics of steel diaphragms for automatic fuel injection valves by W. F. Joachim
Washington, D.C.: NACA, 1926
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The characteristics of the NACA M 12 airfoil section by George J. Higgins
Washington, D.C.: NACA, 1926
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Effect of protruding gasoline tanks upton the characteristics of an airfoil by Eastman N. Jacobs
Washington, D.C.: NACA, 1926
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Resistance of a fifteen centimeter disk by James M. Shoemaker
Washington, D.C.: NACA, 1926
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Propeller design 3 A simple system based on model propeller test data by Fred E. Weick
Washington, D.C.: NACA, 1926
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Tests of several bearing materials lubricated by gasoline by W. F. Joachim and Harold W. Case
Washington, D.C.: NACA, 1926
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Simplified propeller design for low powered airplanes by Fred E. Weick
[Washington, D.C.]: NACA, 1925
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Discharge characteristics of a high speed fuel injection engine by Robertson Matthews
[Washington, D.C.]: NACA, 1925
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Note on the Katzmayr effect on arifoill drag by Shatswell Ober
[Washington, D.C.]: NACA, 1925
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The calculaltion of wing float displacement by Edward P. Warner
[Washington, D.C.]: NACA, 1925
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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
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Note on the air forces on a wing caused by pitching by Max M. Munk
[Washington, D.C.]: NACA, 1925
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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
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Determination and classification of the aerodynamic properties of wing sections by Max M. Munk
Washington, D.C.: NACA, 1925
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An altitude chamber for the study and calibration of aeronautical instruments by J. E. Reid and Otto E. Kirchner
Washington, D.C.: NACA, 1925
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The Flettner rotor ship in the light of the Kutta-Joukowski theory and of experimental results by Frank Rizzo
Washington, D.C.: NACA, 1925
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Aircraft engine design by E. E. Wilson
[Washington, D.C.]: NACA, 1925
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Model tests on the economy and effectiveness of helicopter propellers by Max M. Munk
[Washington, D.C.]: NACA, 1925
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Air flow investigation for lacation of angle of attack head on a JN4h airplane by R. G. Freeman
[Washington, D.C.]: NACA, 1925
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Propeller scale effect and body interference by Fred E. Weick
Washington, D.C.: NACA, 1925
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Wind tunnel tests of fuselages and windshields by Edward P. Warner
Washington, D.C.: NACA, 1925
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Tests on duralumin columns for aircraft construction by John G. Lee
[Washington, D.C.]: NACA, 1924
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Tests of rotating cylinders by Elliot G. Reid
[Washington, D.C.]: NACA, 1924
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The testing of aviation engines under approximate altitude conditions by R. N. DuBois
[Washington, D.C.]: NACA, 1924
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High altitude flying by Paul B. King and Thomas Carroll
[Washington, D.C.]: NACA, 1924
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A method of determining the dimensions and horsepower of an airship for any given performance by C. P. Burgess
[Washington, D.C.]: NACA, 1924
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On the distribution of lift along the span of an airfoil with displaced ailerons by Max M. Munk
[Washington, D.C.]: NACA, 1924
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A short method of calculating torsional stresses in an airplane fuselage by John E. Younger
[Washington, D.C.]: NACA, 1924
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Some tables of the factor of apparent additional mass by Max M. Munk
[Washington, D.C.]: NACA, 1924
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A study of static stability of airships by Frank Rizzo
Washington, D.C.: NACA, 1924
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The logarithmic polar curve - its theory and application to the predetermination of airplane performance by Val Cronstedt
[Washington, D.C.]: NACA, 1924
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Structural weight of aircraft as affected by the system of design by Charles Ward Hall
[Washington, D.C.]: NACA, 1924
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Micarta propellers 4 Technical methods of design by F. W. Caldwell and N. S. Clay
[Washington, D.C.]: NACA, 1924
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Note on the relative effect of the dihedral and the sweep back of airplane wings by Max M. Munk
[Washington, D.C.]: NACA, 1924
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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
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Static stability of seaplane floats and hulls by W. S. Diehl
[Washington, DC]: NACA, 1924
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Note on vortices and on their relation to the lift of airfoils by Max M. Munk
[Washington, D.C.]: NACA, 1924
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The induction factor used for computing the rolling moment due to the allerons by Max M. Munk
[Washington, D.C.]: NACA, 1924
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Comparing the performance of geometrically similar airplanes by Max M. Munk
[Washington, D.C.]: NACA, 1924
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Note on the pressure distribution over the hull of elongated airships with circular cross section by Max M. Munk
[Washington, D.C.]: NACA, 1924
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The effect of wind tunnel turbulence upton the forces measured models by W. L. LePage and J. T. Nichols
[Washington, DC]: NACA, 1924
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Micarta propellers 1 Materials by F. W. Caldwell and N. S. Clay
[Washington, D.C.]: NACA, 1924
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Micarta propellers 2 Method of construction by F. W. Caldwell and N. S. Clay
[Washington, D.C.]: NACA, 1924
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Micarta propellers 3 General description of the design by F. W. Caldwell and N. S. Clay
[Washington, D.C.]: NACA, 1924
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Wind tunnel tests of five strut sections in yaw by Edward P. Warner
[Washington, D.C.]: NACA, 1923
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The Nichols wing cutting equipment by James B. Ford
[Washington, D.C.]: NACA, 1923
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Preliminary study of the damping factor in roll by James M. Shoemaker and John G. Lee
[Washington, D.C.]: NACA, 1923
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Notes on the design of ailerons by W. S. Diehl
[Washington, DC]: NACA, 1923
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Notes o the N.A.C.A. control force recorder by H. J. E. Reid
[Washington, DC]: NACA, 1923
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An instrument for recording the position of airplane control surfaces by K. M. Ronan
[Washington, DC]: NACA, 1923
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Tests on built-up airplane struts having initial tension in outside fibers by T. A. Schwamb and C. S. Smith
[Washington, DC]: NACA, 1923
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An impulse electric motor for driving recording instruments by W. F. Joachim
[Washington, DC]: NACA, 1923
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An optical altitude indicator for night landing by John A. C. Warner
[Washington, DC]: NACA, 1923
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The NACA recording tachometer and angle of attack recorder by H. J. E. Reid
[Washington, DC]: NACA, 1923
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Tests on riveted joints in sheet duralumin by H. F. Rettew and C. Thumin
[Washington, DC]: NACA, 1923
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Measurements of rudder moments on an airplane during flight by Ing. v. Heidelberg
[Washington, D.C.]: NACA, 1921
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Airplane crashes: Engine troubles a possible explanation by Stanwood W. Sparrow
Washington, D.C.: NACA, 1921
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Effect of the reversal of air flow upon the discharge coefficient of Durley orifices by Marsden Ware
[Washington, D.C.]: NACA, 1921
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The determination of downwash by Walter S. Diehl
[Washington, DC]: NACA, 1921
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Causes of cracking of ignition cable by F. B. Silsbee
[Washington, D.C.]: NACA, 1921
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The effect of the nature of surfaces on resistance, as tested on struts by C. Wieselsberger
[Washington, D.C.]: NACA, 1921
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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
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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
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The factors that determine the minimum speed of an airplane by F. H. Norton
[Washington, D.C.]: NACA, 1921
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On the resistance of the air at high speeds and on the automatic rotation of projectiles by D. Riabouchinski
[Washington, D.C.]: NACA, 1921
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On the resistance of spheres and ellipsoids in wind tunnels by D. P. Riabouchinsky
[Washington, DC]: NACA, 1921
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Soaring flight in Guinea by P. Idrac
Washington, D.C.: NACA, 1920
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The problem of the turbo-compressor extract from "The Internal Combustion Engine" by René Devillers
Washington, D.C.: NACA, 1920
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High thermal efficiency in airplane service by S. W. Sparrow
[Washington, D.C.]: NACA, 1920
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The photographic recording of small motions by F. H. Norton
[Washington, D.C.]: NACA, 1920
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Horizontal buoyancy in wind tunnel by A. F. Zahn
[Washington, D.C.]: NACA, 1920
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A variable speed fan dynamometer by Karl D. Wood
[Washington, D.C.]: NACA, 1920
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Progress made in the construction of giant airplanes in germany during the war by A. Baumann
[Washington, D.C.]: NACA, 1920
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Design of recording wind tunnel balances by S. W. Sparrow
[Washington, D.C.]: NACA, 1920
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The steadiness factor in engine sets by W. Margoulis
Washington, D.C.: NACA, 1920
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Notes on specifications for french airplane competitions by W. Margoulis
Washington, D.C.: NACA, 1920
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Italian and French experiments on wind tunnels by Wm. Knight
Washington, D.C.: NACA, 1920
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Increase in maximum pressures produced by preignition in internal combustion engines by S. W. Sparrow
[Washington, D.C.]: NACA, 1920