> Publishers' series
-
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
-
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
-
3241:
Airfoil section characteristics at high angles of attack by Laurence K. Loftin
Washington, DC: National Advisory Committee for Aeronautics, 1954
-
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
-
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
-
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
-
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
-
2661:
A summary of diagonal tension 1 Methods of analysis by Paul Kuhn; James P. Peterson and L. Ross Levin
Washington: NACA, 1952
-
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
-
2743:
Landing-gear impact by W. Flügge
Washington, DC: National Advisory Committee for Aeronautics, 1952
-
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
-
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
-
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
-
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
-
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
-
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]
-
748:
Principles, practice, and progress of noise reduction in airplanes by Albert London
Washington, DC: NACA, 1940
-
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
-
732:
A simple method of obtaining span load distributions by Albert Sherman
Washington, D.C.: NACA, 1939
-
738:
Corrugated metal diaphragms for aircraft pressure measuring instruments by W. A. Wildhack and V. H. Goerke
Washington, D.C.: NACA, 1939
-
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]
-
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]
-
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
-
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
-
705:
Wind tunnel investigation of ground effect on wings with flaps by Isidore G. Recant
Washington, D.C.: NACA, 1939
-
717:
A method of estimating the critical buckling load for structural members by Eugene E. Lundquist
[Washington, DC]: NACA, [1939]
-
722:
Local instability of centrality loaded columns of channel section and Z-section by Eugene E. Lundquist
[Washington, DC]: NACA, [1939]
-
711:
An approximate spin design criterion for monoplanes by Oscar Seidman and Charles J. Donlan
[Washington, DC]: NACA, [1939]
-
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
-
726:
Combined beam column stresses of aluminium alloy channel sections by R. Gottlieb, T. M. Thompson and E. C. Witt
[Washington, DC]: NACA, [1939]
-
737:
Photoelastic analysis of three-dimensional stress systems using scattered light by R. Weller and J. K. Bussey
[Washington, DC]: NACA, [1939]
-
721:
Compressive tests of a monocoque box by Walter Ramberg, Albert E. McPherson, and Sam Levy
[Washington, DC]: NACA, [1939]
-
713:
A comparison of several tapered wings designed to avoid tip stalling by Raymond F. Anderson
[Washington, DC]: NACA, [1939]
-
745:
Tests of a gust alleviating flap in [...] by Philip Donely and C. C. Shufflebarger
Washington, D.C.: NACA, 1939
-
692:
Some fundamental considerations in regard to the use of power in landing an airplane by Walter S. Diehl
[Washington, DC]: NACA, [1939]
-
724:
The effects of surface waviness and of rib stitching on wing drag by Manley J. Hood
[Washington, DC]: NACA, [1939]
-
714:
Flight tests of retractable ailerons on a highly tapered wing by J. W. Wetmore
[Washington, DC]: NACA, [1939]
-
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
-
700:
Theory of automatic control of airplanes by Herbert K. Weiss
Washington, DC: NACA, 1939
-
695:
The effects of some common surface irregula[rities] on wing drag by Manley J. Hood
[Washington, DC]: NACA, [1939]
-
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]
-
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?]
-
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]
-
658:
Generalized analysis of experimental observations in problems of elastic stability by Eugene E. Lundquist
[Washington, DC]: NACA, [1938]
-
649:
The effect of air passage length on the optimum fin spacing for maximum cooling by Maurice J. Brevoort
Washington, DC: NACA, 1938
-
643:
A study of flying boat take-off by Walter S. Diehl
[Washington, DC]: NACA, [1938]
-
636:
The estimation of the rate of change of yawing moment with sideslip by Frederick H. Imlay
[Washington, DC]: NACA, [1938]
-
677:
Tests of a contra-propeller for aircraft by William M. Benson
Washington, DC: NACA, 1938
-
694:
Physical properties of synthetic res[ins] by Meyer Fishbein
[Washington, DC]: NACA, [1938]
-
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]
-
682:
The unsteady lift of a finite wing by Robert T. Jones
[Washington, DC]: NACA, [1938]
-
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]
-
690:
Résumé of air load data on slats and flaps by Carl J. Wenzinger and Francis M. Rogallo
[Washington, DC]: NACA, [1938]
-
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]
-
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]
-
671:
A method of rapidly estimating the position of the laminar separation point by Albert E. von Doenhoff
[Washington, DC]: NACA, [1938]
-
667:
Operational treatment of the nonuniform-lift theory in airplane dynamics by Robert T. Jones
Washington, DC: NACA, 1938
-
645:
Some aspects of the stalling of modern low wing monoplanes by Hartley A. Soulé and Melvin N. Gough
[Washington, DC]: NACA, [1938]
-
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]
-
660:
Fatigue testing of wing beams by the resonance method by William M. Bleakney
[Washington, DC]: NACA, [1938]
-
685:
Circulation measurements about the tip of an airfoil during flight through a gust by Arnold M. Kuethe
[Washington, DC]: NACA, [1938]
-
696:
Torsional stability of aluminium alloy seamless tubing by R. L. Moore and D. A. Paul
[Washington, DC]: NACA, [1938]
-
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
-
520:
Calculations of the effect of wing twist on the air forces acting on a monoplane wing by G. Dätwyler
[Washington, DC]: NACA, [1937?]
-
598:
Wind tunnel tests of a Clark Y wing with "Maxwell" leading edge slots by William E. Gauvain
[Washington, DC]: NACA, [1937]
-
689:
Tandem air propellers by E. P. Lesley
[Washington, D.C.]: NACA, [1937]
-
617:
Stability of structural members under axial load by Eugene E. Lundquist
[Washington, DC]: NACA, [1937]
-
616:
The measurement of air speed of airplanes by F. L. Thompson
[Washington, DC]: NACA, [1937]
-
627:
Pressure distribution over a Clark Y-H airfoil section with a split flap by Carl J. Wenzinger
[Washington, DC]: NACA, [1937]
-
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]
-
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]
-
628:
Plastics as structural materials [...] by G. M. Kline
[Washington, DC]: NACA, [1937]
-
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]
-
623:
Maximum forces applied by pilots to wheel type controls by William H. McAvoy
[Washington, DC]: NACA, [1937]
-
650:
Wind tunnel tests of a Clark Y wing having split flaps with gaps by Carl J. Wenzinger
[Washington, DC]: NACA, [1937]
-
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]
-
589:
Theoretical span loading and moments of tapered wings produced by aileron deflection by H. A. Pearson
Washington, D.C.: NACA, 1937
-
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
-
570:
Effect of changes in tail arrangement upon the spinning of a low wing monoplane [model] by C. H. Zimmerman
[Washington, DC]: NACA, [1936]
-
566:
Tank tests of a model of the NC flying boat hull - NACA model 44 by Joe W. Bell
[Washington, DC]: NACA, [1936]
-
746:
The frequencies of cantilever wings in beam and torsional vibration by C. P. Burgess
Washington, D.C.: NACA, 1936
-
555:
Piloting technique for recovery from spins by W. H. McAvoy
[Washington, DC]: NACA, [1936]
-
562:
Remarks on the elastic axis of shell wings by Paul Kuhn
Washington, D.C.: NACA, 1936
-
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
-
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
-
553:
Notes on the technique of landing airplanes equipped with wing flaps by Melvin N. Gough
[Washington, DC]: NACA, [1936]
-
586:
The reduction of aileron operating force by differential linkage by Robert T. Jones and Albert I. Nerken
Washington, D.C.: NACA, 1936
-
557:
Considerations of the take-off problem by Edwin P. Hartman
[Washington, DC]: NACA, [1936]
-
543:
The compressibility burble by John Stack
[Washington, DC]: NACA, [1935]
-
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
-
539:
Aerodynamic characteristics of several airfoils of low aspect ratio by C. H. Zimmerman
[Washington, DC]: NACA, [1935]
-
547:
Development of the NACA slot lip [aileron] by Fred E. Weick and Joseph [A. Shortal]
[Washington, DC]: NACA, [1935]
-
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]
-
468:
A study of factors affecting the steady spin of an airplane by Nathan F. Scudder
[Washington, DC]: NACA, [1935]
-
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
-
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]
-
523:
Strength tests of thin walled duralumin cylinders in combined transverse shear and bending by Eugene E. Lundquist
Washington, D.C.: NACA, 1935
-
530:
Bending stresses due to torsion in cantile[ver box beams] by Paul Kuhn
[Washington]: NACA, [1935]
-
542:
The initial torsional stiffness of shells with interior webs by Paul Kuhn
[Washington]: NACA, [1935]
-
552:
Wind tunnel tests of wing flaps suitable for direct control of glide-fath angle by Fred E. Weick
[Washington, DC]: NACA, [1935]
-
527:
Strength tests of thin walled duralumin cylinders of elliptic section by Eugene E. Lundquist and Walter F. Burke
Washington, D.C.: NACA, 1935
-
568:
Calculated effect of various types of flap on take-off over obstacles by J. W. Wetmore
[Washington, DC]: NACA, [1935]
-
548:
Flight tests of a balanced split flap with particular reference to rapid operation by H. A. Soule
[Washington, DC]: NACA, [1935]
-
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
-
503:
Measurement of altitude in blind flying by W. G. Brombacher
Washington, D.C.: NACA, 1934
-
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
-
500:
The torsional stiffness of thin duralumin shells subjected to large torques by Paul Kuhn
Washington, D.C.: NACA, 1934
-
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
-
499:
Effect of retractable spoiler location on rolling and yawing moment coefficients by J. A. Shortal
[Washington, DC]: NACA, [1934]
-
509:
Thank tests of flat and V bottom planing surfaces by James M. Shoemaker
Washington, D.C.: NACA, 1934
-
515:
Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model by J. M. Bamber
Washington, D.C.: NACA, 1934
-
484:
A method of calculating the performance of controllable propellers, with sample computations by Edwin P. Hartman
Washington, D.C.: NACA, 1934
-
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]
-
506:
Experimental verification of Theodorsen's theoretical jet boundary correction factors by George Van Schliestett
Washington, D.C.: NACA, 1934
-
508:
Landing characteristics of an autogiro by William C. Peck
[Washington, DC]: NACA, [1934]
-
495:
Effect of the surface condition of a wing on the aerodynamic characteristics of an airplane by S. J. DeFrance
[Washington, DC]: NACA, [1934]
-
501:
Landing shock recorder by Maurice J. Brevoort
[Washington, DC]: NACA, 1934
-
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
-
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
-
513:
The wave suppressors used in the N.A.C.A. tank by Starr Truscott
Washington, D.C.: NACA, 1934
-
502:
Aerodynamic investigation of a cup anemometer by John D. Hubbard and George P. Brescoll
Washington, D.C.: NACA, 1934
-
497:
Full scale drag tests of landing lamps by C. H. Dearborn
Washington, D.C.: NACA, 1934
-
498:
Wind tunnel measurements of air loads on split flaps by Carl J. Wenzinger
Washington, D.C.: NACA, 1934
-
511:
A study of the pitching moments and the stability characteristics of monoplanes by George J. Higgins
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]
-
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
-
467:
Simplified aerodynamic analysis of the cyclogiro rotating wing sys[tem] by John B. Wheatley
[Washington, DC]: NACA, [1933]
-
528:
Wind tunnel tests of a cyclogiro rotor by John B. Wheatley and Ray Windler
[Washington, DC]: NACA, [1933]
-
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]
-
452:
The importance of auto ignition lag in knocking by E. S. Taylor
Washington, D.C.: NACA, 1933
-
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
-
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
-
466:
Engine performance with a hydrogenated safety fuel by Oscar W. Schey and Alfred W. Young
Washington, D.C.: NACA, 1933
-
479:
Strength test of thin walled duralu[min cylinders] in pure bending by Eugene E. Lundquist
[Washington, DC]: NACA, [1933]
-
481:
The reduction in drag of a forward sloping windshield by Eastman N. Jacobs
[Washington, DC]: NACA, [1933]
-
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]
-
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
-
442:
Jet propulsion with special reference to thrust augmentors by G. B. Schubauer
Washington, D.C.: NACA, 1933
-
446:
Estimation of the variation of thrust horsepower with air speed by Shatswell Ober
Washington, D.C.: NACA, 1933
-
448:
Effect of aileron displacement on wing characteristics by R. H. Heald
Washington, D.C.: NACA, 1933
-
450:
Mercerization of cotton for strength with special reference to aircraft cloth by J. B. Wilkie
Washington, D.C.: NACA, 1933
-
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
-
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
-
480:
The drag of streamline wires by Eastman N. Jacobs
[Washington, DC]: NACA, [1933]
-
453:
Experiments with a counter propeller by E. P. Lesley
Washington, D.C.: NACA, 1933
-
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
-
456:
The aerodynamic effect of a retractable landing gear by Smith J. DeFrance
Washington, D.C.: NACA, 1933
-
465:
Some characteristics of sprays obtained from pintle type injection nozzles by E. T. Marsh and C. D. Waldron
Washington, D.C.: NACA, 1933
-
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
-
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
-
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
-
457:
The aerodynamic characteristics of airfoils as affected by surface roughness by Ray W. Hocker
Washington, D.C.: NACA, 1933
-
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
-
474:
Effect of stabilizer [...] by M. J. Bamber
[Washington, D.C.]: NACA, [ca. 1933]
-
483:
Charts for determining the pitching moment of tapered wings with sweepback and twist by Raymond F. Anderson
Washington, D.C.: NACA, 1933
-
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
-
405:
Valve timing of engines having intake pressures higher than exhaust by Edward S. Taylor
Washington, D.C.: NACA, 1932
-
424:
Preliminary photomicrographic studies of fuel sprays by Dana W. Lee and Robert C. Spencer
Washington, D.C.: NACA, 1932
-
420:
The effect of propellers and nacelles on the landing speeds of tractor monoplanes by Ray Windler
Washington, D.C.: NACA, 1932
-
417:
Wind tunnel tests of a hall high lift wing by Fred E. Weick and Robert Sanders
Washington, D.C.: NACA, 1932
-
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
-
412:
The aerodynamic characteristics of airfoils at negative angles of attack by Raymond F. Anderson
Washington, D.C.: NACA, 1932
-
432:
Drag tests of 4 9 scale model engine nacelles with various cowlings by Ray Windler
Washington, D.C.: NACA, 1932
-
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
-
418:
Compression ignition engine tests of several fuels by J. A. Spanogle
Washington, D.C.: NACA, 1932
-
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
-
439:
Meteorological conditions during the formation of ice on aircraft by L. T. Samuels
Washington, D.C.: NACA, 1932
-
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
-
413:
The compressive strength of duralumin columns of equal angle section by Eugene E. Lundquist
Washington, D.C.: NACA, 1932
-
427:
Strength tests on thin walled duralumin cylinders in torsion by Eugene E. Lundquist
Washington, D.C.: NACA, 1932
-
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
-
410:
Experiments on the distribution of fuel in fuel sprays by Dana W. Lee
Washington, D.C.: NACA, 1932
-
419:
Wind tunnel tests of the fowler variable area wing by Fred E. Weick and Robert C. Platt
Washington, D.C.: NACA, 1932
-
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
-
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
-
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
-
428:
Characteristics of an airfoil as affected by fabric sag by Kenneth E. Ward
[Washington, DC]: NACA, [1932]
-
425:
Methods of visually determining the air flow around airplanes by Melvin N. Gough and Ernest Johnson
[Washington, DC]: NACA, [1932]
-
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
-
437:
The pressure distribution over a long elliptical wing tip on a biplane in flight by Richard V. Rhode
Washington, D.C.: NACA, 1932
-
408:
Preliminary tests on the vaporization of fuel sprays by A. M. Rothrock
Washington, D.C.: NACA, 1932
-
444:
Working charts for the stress analysis [of elliptic rings] by Walter F. Burke
[Washington, DC]: NACA, 1932
-
399:
Some characteristics of fuel sprays at low injection pressures by A. M. Rothrock and C. D. Waldron
Washington, D.C.: NACA, 1931
-
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
-
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
-
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
-
377:
An integrating manometer for use in wind tunnel pressure distribution measurements by Richard W. Noyes
Washington, D.C.: NACA, 1931
-
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
-
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
-
366:
Torsion in box wings by John B. Wheatley
Washington, D.C.: NACA, 1931
-
368:
The variation in pressure in the cabin of an airplane in flight by Melvin N. Gough
Washington, D.C.: NACA, 1931
-
385:
Tests of six symmetrical airfoils in the variable density wind tunnel by Easrman N. Jacobs
Washington, D.C.: NACA, 1931
-
386:
Effect of nose shape on characteristics of symmetrical airfoils by Robert M. Pinkerton
Washington, D.C.: NACA, 1931
-
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]
-
383:
Metal truss wing spars by Andrew E. Swickard
Washington, D.C.: NACA, 1931
-
416:
Characteristics of two sharp nosed airfoils having reduced spinning tendencies by Eastman N. Jacobs
[Washington, DC]: NACA, [1931]
-
361:
The effect of small variations in profile of airfoils by Kenneth E. Ward
Washington, D.C.: NACA, 1931
-
363:
The behavior of conventional airplanes in situations thought to lead to most crashes by Fred E. Weick
Washington, D.C.: NACA, 1931
-
365:
Interference effects and drag of struts on a monoplane wing by Kenneth E. Ward
Washington, D.C.: NACA, 1931
-
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
-
390:
A method for reducing the temperature of exhaust manifolds by Oscar W. Schey and Alfred W. Young
Washington, D.C.: NACA, 1931
-
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
-
378:
Comparison of weights of 17ST and steel tubular structural members used in aircraft construction by E. C. Hartmann
Washington, D.C.: NACA, 1931
-
382:
Basic requirements of fuel injection nozzles for quiescent combustion chambers by J. A. Spanogle and H. H. Foster
Washington, D.C.: NACA, 1931
-
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
-
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
-
380:
A suggested method for measuring turbulence by C. Fayette Taylor
Washington, D.C.: NACA, 1931
-
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
-
367:
The aerodynamic characteristics of three tapered airfoils tested in the variable density wind tunnel by John B. Wheatley
Washington, D.C.: NACA, 1931
-
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
-
375:
Moments of inertia of airplanes by Marvel P. Miller and Hartley A. Soulé
Washington, D.C.: NACA, 1931
-
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
-
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
-
403:
The interference effects on an airfoil of a flat plate at mid span position by Kenneth E. Ward
Washington, D.C.: NACA, 1931
-
376:
Effect of high air velocities on the distribution and penetration of a fuel spray by A. M. Rothrock
Washington, D.C.: NACA, 1931
-
393:
An investigation of cotton for parachute cloth by Wm. D. Appel and R. K. Worner
Washington, D.C.: NACA, 1931
-
394:
The prevention of ice formation on gasoline tank vents by Theodore Theodorsen and William C. Clay
Washington, D.C.: NACA, 1931
-
395:
Penetration and duration of fuel sprays from pump injection system by A. M. Rothrock and E. T. Marsh
Washington, D.C.: NACA, 1931
-
351:
An accurate method of measuring the moments of inertia of airplanes by M. P. Miller
Washington, D.C.: NACA, 1930
-
349:
An investigation of airplane landing speeds by Kenneth F. Ridley
Washington, D.C.: NACA, 1930
-
338:
Some effects of air and fuel oil temperatures on spray penetration and dispersion by A. G. Gelalles
Washington, D.C.: NACA, 1930
-
345:
The prevention of the ice hazard on airplanes by William C. Geer and Merit Scott
Washington, D.C.: NACA, 1930
-
333:
Test of an adjustable pitch model propeller at four blade settings by E. P. Lesley
Washington, D.C.: NACA, 1930
-
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
-
332:
Injection lags in a common rail fuel injection system by A. M. Rothrock
Washington, D.C.: NACA, 1930
-
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
-
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
-
335:
The structure and properties of parachute cloths by H. J. McNicholas and A. F. Hedrick
Washington, D.C.: NACA, 1930
-
348:
Alterations and tests of the "Farnboro" engine indicator by John H. Collins
Washington, D.C.: NACA, 1930
-
356:
Some characteristics of fuel sprays from open nozzles by A. M. Rothrock and D. W. Lee
Washington, D.C.: NACA, 1930
-
357:
Bending tests of metal monocoque fuselage construction by Ralph W. Mossman and Russell G. Robinson
Washington, D.C.: NACA, 1930
-
352:
Effect of orifice length diameter ratio on spray characteristics by A. G. Gelalles
Washington, D.C.: NACA, 1930
-
353:
Analytical determination of the load on a trailing dege flap by Robert M. Pinkerton
Washington, D.C.: NACA, 1930
-
342:
Identification of aircraft tubing by rockwell test by Horace Knerr
Washington, D.C.: NACA, 1930
-
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
-
337:
Pressure distribution on the tail surfaces of a PW-9 pursuit airplane in flight by Richard V. Rhode
Washington, D.C.: NACA, 1930
-
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
-
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
-
317:
Tests of four racing type airfoils in the twenty-foot propeller research tunnel by Fred E. Weick
Washington, D.C.: NACA, 1929
-
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
-
302:
A new method for the prediction of airplane performance by E. P. Lesley and E. G. Reid
Washington, D.C.: NACA, 1929
-
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
-
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
-
321:
The impact on seaplane floats during landing by Th. von Karman
Washington, D.C.: NACA, 1929
-
303:
Condensed data on the aircraft engines of the world compiled by C. S. Fliedner
Washington, D.C.: NACA, 1929
-
304:
Corrosion embrittlement of duralumin 5 The results of weather exposure tests by Henry S. Rawdon
Washington, D.C.: NACA, 1929
-
319:
Some experiments on autorotation of an airfoil by Shatswell Ober
Washington, D.C.: NACA, 1929
-
318:
Full scale investigation of the drag of a wing radiator by Fred E. Weick
Washington, D.C.: NACA, 1929
-
313:
The formation of ice upon airplanes in flight by Thomas Carroll and William H. MacAvoy
Washington, D.C.: NACA, 1929
-
327:
Some studies on the aerodynamic effect of the gap between airplane wings and fuselages by Shatswell Ober
Washington, D.C.: NACA, 1929
-
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
-
306:
Curves showing column strength of steel and duralumin tubing by Orrin E. Ross
Washington, D.C.: NACA, 1929
-
314:
Spiral tendency in blind flying by Thomas Carroll and William H. MacAvoy
Washington, D.C.: NACA, 1929
-
315:
Viscosity of diesel engine fuel oil under pressure by Mayo D. Hersey
Washington, D.C.: NACA, 1929
-
320:
The drag and interference of a nacelle in the presence of a wing by Eastman N. Jacobs
Washington, D.C.: NACA, 1929
-
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
-
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
-
282:
Corrosion embrittlement of duralumin 1 Practical aspects of the problem by Henry S. Rawdon
Washington, D.C.: NACA, 1928
-
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
-
291:
Gluing practice at aircraft manufacturing plants and replair stations by T. R. Truax
Washington, D.C.: NACA, 1928
-
485:
Research on the control of airplanes by B. Melvill Jones
Washington, D.C.: NACA, 1928
-
279:
Resistance of streamline wires by George L. DeFoe
Washington, D.C.: NACA, 1928
-
280:
Drag of exposed fittings and surface irregularities on airplane fuselages by Donald H. Wood
Washington, D.C.: NACA, 1928
-
287:
A dangerous seaplane landing condition by Thomas Carroll
Washington, D.C.: NACA, 1928
-
290:
Welding of high chromium steels by W. B. Milller
Washington, D.C.: NACA, 1928
-
490:
Structures of thin sheet metal their design and construction by Herbert Wagner
Washington, D.C.: NACA, 1928
-
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
-
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
-
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
-
276:
Helium tables by Clinton H. Havill
Washington, D.C.: NACA, 1928
-
271:
Full scale drag tests on variuos parts of Sperry Messenger airplane by Fred E. Weick
Washington, D.C.: NACA, 1928
-
292:
The drag of a J 5 radial air cooled engine by Fred E. Weick
Washington, D.C.: NACA, 1928
-
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
-
273:
The effect on performance of a cutaway center section by Thomas Carroll
Washington, D.C.: NACA, 1928
-
275:
Determination of propeller deflection by means of static load tests on models by Fred E. Weick
Washington, D.C.: NACA, 1928
-
272:
Special propeller protractor by A. L. Heim
Washington, D.C.: NACA, 1928
-
278:
An automatic speed sontrol for wind tunnels by A. F. Zahm
Washington, D.C.: NACA, 1928
-
285:
Corrosion embrittlement of duralumin 4 The use of protective coatings by Henry S. Rawdon
Washington, D.C.: NACA, 1928
-
289:
Preliminary biplane tests in the variable density wind tunnel by James M. Shoemaker
Washington, D.C.: NACA, 1928
-
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
-
288:
The reaction on a float bottom when making contact with water at high speeds by H. C. Richardson
Washington, D.C.: NACA, 1928
-
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
-
257:
Technical preparation of the airplane "Spirit of St. Louis" by Donald A. Hall
Washington, D.C.: NACA, 1927
-
254:
Method of correcting wind tunnel data for omitted parts of airplane models by R. H. Smith
Washington, D.C.: NACA, 1927
-
265:
Measurement of the moments of inertia of full scale airplanes by M. W. Green
Washington, D.C.: NACA, 1927
-
269:
The distribution of loads between the wings of a biplane having decalage by Richard M. Mock
Washington, D.C.: NACA, 1927
-
266:
Airfoil lift with changing angle of attack by Elliott G. Reid
Washington, D.C.: NACA, 1927
-
258:
A warning concerting the take-off with heavy load by Elliott G. Reid and Thomas Carroll
Washington, D.C.: NACA, 1927
-
255:
Precision of wing sections and consequent aerodynamic effects by Frank Rizzo
Washington, D.C.: NACA, 1927
-
259:
"Alclad" a new corroion resistant aluminium product by E. H. Dix
Washington, D.C.: NACA, 1927
-
260:
Study of open jet wind tunnel cones by Fred Weick
Washington, D.C.: NACA, 1927
-
261:
Tension experiments on diaphram metals by H. B. Henrickson
Washington, D.C.: NACA, 1927
-
263:
A load factor formula by Roy G. Miller
Washington, D.C.: NACA, 1927
-
264:
Tests of the N.P.L. airship models in the variable density wind tunnel by George J. Higgins
Washington, D.C.: NACA, 1927
-
230:
The spacing of orifices for the measurement of pressure distributions by Max M. Munk
Washington, D.C.: NACA, 1926
-
232:
The lateral failure of spars Stevens Bromley and William H. Robinson
Washington, D.C.: NACA, 1926
-
248:
The drag of airships 2 Drag of bare hulls by Clinton H. Havill
Washington, D.C.: NACA, 1926
-
231:
The resistance to the steady motion of small spheres in fluids by R. A. Castleman
[Washington, D.C.]: NACA, 1926
-
235:
Propeller design 1 Practical application of the blade element theory by Fred E. Weick
Washington, D.C.: NACA, 1926
-
249:
Effect of protruding gasoline tanks upton the characteristics of an airfoil by Eastman N. Jacobs
Washington, D.C.: NACA, 1926
-
243:
The characteristics of the NACA M 12 airfoil section by George J. Higgins
Washington, D.C.: NACA, 1926
-
252:
Resistance of a fifteen centimeter disk by James M. Shoemaker
Washington, D.C.: NACA, 1926
-
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
-
237:
Propeller design 3 A simple system based on model propeller test data by Fred E. Weick
Washington, D.C.: NACA, 1926
-
241:
Tests of several bearing materials lubricated by gasoline by W. F. Joachim and Harold W. Case
Washington, D.C.: NACA, 1926
-
242:
Improving the performance of a compression ignition engine by directing flow of the inlet air by Carlton Kemper
[Washington, D.C.]: NACA, 1926
-
246:
Test of a model propeller with symmetrical blade sections by E. P. Lesley
[Washington, D.C.]: NACA, 1926
-
240:
The NACA CYH airfoil section by George J. Higgins
Washington, D.C.: NACA, 1926
-
233:
NACA flight path angle and air speed recorder by Donald G. Coleman
Washington, D.C.: NACA, 1926
-
244:
Navy propeller section characteristics as used in propeller design by Fred E. Weick
Washington, D.C.: NACA, 1926
-
238:
Propeller design 4 A simple method for determining the strength of propellers by Fred E. Weick
Washington, D.C.: NACA, 1926
-
234:
An investigation of the characteristics of steel diaphragms for automatic fuel injection valves by W. F. Joachim
Washington, D.C.: NACA, 1926
-
213:
Discharge characteristics of a high speed fuel injection engine by Robertson Matthews
[Washington, D.C.]: NACA, 1925
-
214:
Note on the Katzmayr effect on arifoill drag by Shatswell Ober
[Washington, D.C.]: NACA, 1925
-
215:
The calculaltion of wing float displacement by Edward P. Warner
[Washington, D.C.]: NACA, 1925
-
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
-
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
-
227:
Determination and classification of the aerodynamic properties of wing sections by Max M. Munk
Washington, D.C.: NACA, 1925
-
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
-
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
-
222:
Air flow investigation for lacation of angle of attack head on a JN4h airplane by R. G. Freeman
[Washington, D.C.]: NACA, 1925
-
221:
Model tests on the economy and effectiveness of helicopter propellers by Max M. Munk
[Washington, D.C.]: NACA, 1925
-
225:
Propeller scale effect and body interference by Fred E. Weick
Washington, D.C.: NACA, 1925
-
226:
Wind tunnel tests of fuselages and windshields by Edward P. Warner
Washington, D.C.: NACA, 1925
-
211:
Aircraft engine design by E. E. Wilson
[Washington, D.C.]: NACA, 1925
-
217:
Note on the air forces on a wing caused by pitching by Max M. Munk
[Washington, D.C.]: NACA, 1925
-
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
-
212:
Simplified propeller design for low powered airplanes by Fred E. Weick
[Washington, D.C.]: NACA, 1925
-
193:
High altitude flying by Paul B. King and Thomas Carroll
[Washington, D.C.]: NACA, 1924
-
204:
A study of static stability of airships by Frank Rizzo
Washington, D.C.: NACA, 1924
-
305:
The logarithmic polar curve - its theory and application to the predetermination of airplane performance by Val Cronstedt
[Washington, D.C.]: NACA, 1924
-
206:
Structural weight of aircraft as affected by the system of design by Charles Ward Hall
[Washington, D.C.]: NACA, 1924
-
184:
Note on vortices and on their relation to the lift of airfoils by Max M. Munk
[Washington, D.C.]: NACA, 1924
-
191:
The effect of wind tunnel turbulence upton the forces measured models by W. L. LePage and J. T. Nichols
[Washington, DC]: NACA, 1924
-
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
-
187:
The induction factor used for computing the rolling moment due to the allerons by Max M. Munk
[Washington, D.C.]: NACA, 1924
-
190:
Comparing the performance of geometrically similar airplanes by Max M. Munk
[Washington, D.C.]: NACA, 1924
-
183:
Static stability of seaplane floats and hulls by W. S. Diehl
[Washington, DC]: NACA, 1924
-
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
-
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
-
198:
Micarta propellers 1 Materials by F. W. Caldwell and N. S. Clay
[Washington, D.C.]: NACA, 1924
-
199:
Micarta propellers 2 Method of construction by F. W. Caldwell and N. S. Clay
[Washington, D.C.]: NACA, 1924
-
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
-
200:
Micarta propellers 3 General description of the design by F. W. Caldwell and N. S. Clay
[Washington, D.C.]: NACA, 1924
-
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
-
195:
On the distribution of lift along the span of an airfoil with displaced ailerons by Max M. Munk
[Washington, D.C.]: NACA, 1924
-
203:
A short method of calculating torsional stresses in an airplane fuselage by John E. Younger
[Washington, D.C.]: NACA, 1924
-
201:
Micarta propellers 4 Technical methods of design by F. W. Caldwell and N. S. Clay
[Washington, D.C.]: NACA, 1924
-
208:
Tests on duralumin columns for aircraft construction by John G. Lee
[Washington, D.C.]: NACA, 1924
-
209:
Tests of rotating cylinders by Elliot G. Reid
[Washington, D.C.]: NACA, 1924
-
210:
The testing of aviation engines under approximate altitude conditions by R. N. DuBois
[Washington, D.C.]: NACA, 1924
-
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
-
197:
Some tables of the factor of apparent additional mass by Max M. Munk
[Washington, D.C.]: NACA, 1924
-
123:
An optical altitude indicator for night landing by John A. C. Warner
[Washington, DC]: NACA, 1923
-
165:
Tests on riveted joints in sheet duralumin by H. F. Rettew and C. Thumin
[Washington, DC]: NACA, 1923
-
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
-
144:
Notes on the design of ailerons by W. S. Diehl
[Washington, DC]: NACA, 1923
-
156:
The NACA recording tachometer and angle of attack recorder by H. J. E. Reid
[Washington, DC]: NACA, 1923
-
157:
An impulse electric motor for driving recording instruments by W. F. Joachim
[Washington, DC]: NACA, 1923
-
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
-
161:
Preliminary study of the damping factor in roll by James M. Shoemaker and John G. Lee
[Washington, D.C.]: NACA, 1923
-
172:
The Nichols wing cutting equipment by James B. Ford
[Washington, D.C.]: NACA, 1923
-
150:
Notes o the N.A.C.A. control force recorder by H. J. E. Reid
[Washington, DC]: NACA, 1923
-
154:
An instrument for recording the position of airplane control surfaces by K. M. Ronan
[Washington, DC]: NACA, 1923
-
167:
Wind tunnel tests of five strut sections in yaw by Edward P. Warner
[Washington, D.C.]: NACA, 1923
-
33:
The effect of the nature of surfaces on resistance, as tested on struts by C. Wieselsberger
[Washington, D.C.]: NACA, 1921
-
54:
The factors that determine the minimum speed of an airplane by F. H. Norton
[Washington, D.C.]: NACA, 1921
-
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
-
42:
The determination of downwash by Walter S. Diehl
[Washington, DC]: NACA, 1921
-
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
-
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
-
38:
Measurements of rudder moments on an airplane during flight by Ing. v. Heidelberg
[Washington, D.C.]: NACA, 1921
-
55:
Airplane crashes: Engine troubles a possible explanation by Stanwood W. Sparrow
Washington, D.C.: NACA, 1921
-
40:
Effect of the reversal of air flow upon the discharge coefficient of Durley orifices by Marsden Ware
[Washington, D.C.]: NACA, 1921
-
32:
Causes of cracking of ignition cable by F. B. Silsbee
[Washington, D.C.]: NACA, 1921
-
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
-
44:
On the resistance of spheres and ellipsoids in wind tunnels by D. P. Riabouchinsky
[Washington, DC]: NACA, 1921
-
11:
The problem of the turbo-compressor extract from "The Internal Combustion Engine" by René Devillers
Washington, D.C.: NACA, 1920
-
13:
Soaring flight in Guinea by P. Idrac
Washington, D.C.: NACA, 1920
-
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
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22:
The photographic recording of small motions by F. H. Norton
[Washington, D.C.]: NACA, 1920
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26:
A variable speed fan dynamometer by Karl D. Wood
[Washington, D.C.]: NACA, 1920
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29:
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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17:
Italian and French experiments on wind tunnels by Wm. Knight
Washington, D.C.: NACA, 1920
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39:
High thermal efficiency in airplane service by S. W. Sparrow
[Washington, D.C.]: NACA, 1920
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23:
Horizontal buoyancy in wind tunnel by A. F. Zahn
[Washington, D.C.]: NACA, 1920
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30:
Design of recording wind tunnel balances by S. W. Sparrow
[Washington, D.C.]: NACA, 1920
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14:
Increase in maximum pressures produced by preignition in internal combustion engines by S. W. Sparrow
[Washington, D.C.]: NACA, 1920
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19:
The steadiness factor in engine sets by W. Margoulis
Washington, D.C.: NACA, 1920
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20:
Notes on specifications for french airplane competitions by W. Margoulis
Washington, D.C.: NACA, 1920