United States, National Advisory Committee for Aeronautics
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United States, National Advisory Committee for Aeronautics
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United States
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National Advisory Committee for Aeronautics
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Incoming Resources
- 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
- Note on the Katzmayr effect on airfoil drag, by Shatswell Ober
- Local instability of symmetrical rectangular tubes under axial compression, by Eugene E. Lundquist
- Meteorological conditions during the formation of ice on aircraft, by L.T. Samuels
- Tests of N.A.C.A. airfoils in the variable density wind tunnel, by Eastman N. Jacobs and Robert M. Pinkerton
- Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0° to 180°, by Chris C. Critzos, Harry H. Heyson, and Robert W. Boswinkle, Jr
- Jet propulsion with special reference to thrust augmentors, by G.B. Schubauer
- Some investigations of the general instability of stiffened metal cylinders, by Louis G. Dunn, VIII
- Principal effects of axial load on moment-distribution analysis of rigid structures, by Benjamin Wylie James
- Wind-tunnel research comparing lateral control devices, particularly at high angles of attack, by Fred E. Weick and Richard W. Noyes, X
- Theory of ground vibrations of a two-blade helicopter rotor on anisotropic flexible supports, by Robert P. Coleman and Arnold M. Feingold
- The determination of the angles of attack of zero lift and of zero moment, based on Munk's integrals, by Max M. Munk
- Wind-tunnel investigation of ground effect on wings with flaps, by Isidore G. Recant
- Experimental study of torsional column failure, by Alfred S. Niles
- Aerodynamic investigation of a cup anemometer, by John D. Hubbard and George P. Brescoll
- The determination of downwash, by Walter S. Diehl
- Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range, by Dean R. Chapman
- Influence of span and load per square meter on the air forces of the supporting surface, by A. Betz
- Notes on the standard atmosphere, by Walter S. Diehl
- Wind tunnel pressure distribution tests on an airfoil with trailing edge flap, by Carl J. Wenzinger and Oscar Loeser, Jr
- Effect of orifice length-diameter ratio on spray characteristics, by A. G. Gelalles
- Flight tests to determine the effect of a fixed auxiliary airfoil on the lift and drag of a parasol monoplane, by Hartley A. Soulé
- A general tank test of a model of the hull of the British Singapore IIC flying boat, by John R. Dawson and Starr Truscott
- Tandem air propellers, by E.P. Lesley
- Effect of rivet and spot-weld spacing on the strength of axially loaded sheet-stringer panels of 24S-T aluminum alloy, by Samuel Levy, Albert E. McPherson, and Walter Ramberg
- Notes on the theory of the accelerometer, by E.P. Warner
- Relief of residual stress in streamline tie rods by heat treatment, by R.E. Pollard and Fred M. Reinhart
- Aerodynamics of slender wings and wing-body combinations having swept trailing edges, by Harold Mirels
- Wind tunnel standardization disk drag, by Montgomery Knight
- The effect of trim angle on the take-off performance of a flying boat, by James M. Shoemaker and John R. Dawson
- Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7, by M. J. Turner and S. Rabinowitz
- The effect of tube length upon the recorded pressures from a pair of static orifices in a wing panel, by T. Carroll and R.E. Mixon
- A comparison of the results from general tank tests of 1/6- and 1/12-full-size models of the British Singapore IIC flying boat, by Starr Truscott and John R. Dawson
- Wind-tunnel tests of wing flaps suitable for direct control of glide-path angle, by Fred E. Weick
- The dynamometer hub for testing propellers and engines during flight, by O. Enoch
- Aerodynamic characteristics of a number of modified NACA four-digit-series airfoil sections, by Laurence K. Loftin, Jr. and Kenneth S. Cohen
- Tests of four racing type airfoils in the twenty-foot propeller research tunnel, by Fred E. Weick
- Plate method of ground representation for wind-tunnel determination of elevator effectiveness in landing, by I.G. Recant
- Comparison of weights of 17ST and steel tubular structural members used in aircraft construction, by E.C. Hartmann
- Notes on the stalling of vertical tail surfaces and on fin design, by F.L. Thompson and R.R. Gilruth
- Results of landing tests of various airplanes, by J.A. Hootman and A.R. Jones
- The installation and correction of compasses in airplanes, by M.F. Schoeffel
- An instrument for recording the position of airplane control surfaces, by K.M. Ronan
- A new method of testing models in wind tunnels, by W. Margoulis
- Stability of structural members under axial load, by Eugene E. Lundquist
- The importance of auto-ignition lag in knocking, by E.S. Taylor
- Analysis and comparison with theory of flow-field measurements near a lifting rotor in the Langley full-scale tunnel, by Harry H. Heyson
- Wind-tunnel tests of a wing with a trailing-edge auxiliary airfoil used as a flap, by Richard W. Noyes
- Is there any available source of heat energy lighter than gasoline?, by P. Meyer
- The factors that determine the minimum speed of an airplane, by F.H. Norton
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- United States, National Advisory Committee for Aeronautics -- Bibliography
- United States, National Advisory Committee for Aeronautics -- History
- United States, National Advisory Committee for Aeronautics -- Medals
- United States, National Advisory Committee for Aeronautics -- Periodicals
- United States, National Advisory Committee for Aeronautics -- Insignia
- Notes on the theory of the accelerometer, by E.P. Warner
- Loads and calculations of Army airplanes, by Ing. Stelmachowski
- Effect of rivet and spot-weld spacing on the strength of axially loaded sheet-stringer panels of 24S-T aluminum alloy, by Samuel Levy, Albert E. McPherson, and Walter Ramberg
- Measured moments of inertia of 32 airplanes, by William Gracey
- Bending with large deflection of a clamped rectangular plate with length-width ratio of 1.5 under normal pressure, by Samuel Levy and Samuel Greenman
- Notes on the theoretical characteristics of two-dimensional supersonic airfoils, H. Reese Ivey
- Notes on propeller design, by Max M. Munk, IV
- Complete tank tests of two flying-boat hulls with pointed steps - N.A.C.A. Models 22-A and 35, by James M. Shoemaker and Joe W. Bell
- 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
- Note on the relative effect of the dihedral and the sweep back of airplane wings, by Max M. Munk
- Jet propulsion with special reference to thrust augmentors, by G.B. Schubauer
- Note on the Katzmayr effect on airfoil drag, by Shatswell Ober
- The compressibility burble, by John Stack
- Flight tests of retractable ailerons on a highly tapered wing, by J.W. Wetmore
- The compressive yield strength of extruded shapes of 24ST aluminum alloy, by R.L. Templin, F.M. Howell, and E.C. Hartmann
- Wind tunnel pressure distribution tests on an airfoil with trailing edge flap, by Carl J. Wenzinger and Oscar Loeser, Jr
- The N.A.C.A. optical engine indicator, by Robert E. Tozier
- Acoustical treatment for the NACA 8- by 6-foot supersonic propulsion wind tunnel, by Leo L. Beranek, Samuel Labate, and Uno Ingard
- Aerodynamic effects caused by icing of an unswept NACA 65A004 airfoil, by Vernon H. Gray and Uwe H. von Glahn
- Notes on the standard atmosphere, by Walter S. Diehl
- Plastics as structural materials for aircraft, by G.M. Kline
- Instrument for measuring engine clearance volumes, by S.W. Sparrow
- A general tank test of a model of the hull of the British Singapore IIC flying boat, by John R. Dawson and Starr Truscott
- Center of pressure coefficients for airfoils at high speeds, by W.S. Diehl
- Measurement of the forces acting on gliders in towed flight, by W.B. Klemperer
- Strength tests of thin-walled duralumin cylinders in pure bending, by Eugene E. Lundquist
- Tandem air propellers, by E.P. Lesley
- Effect of spark-timing regularity on the knock limitations of engine performance, by Arnold E. Biermann
- Aerodynamic interference of slender wing-tail combinations, by Alvin H. Sacks
- Analysis and model tests of autogiro jump take-out, by John B. Wheatley and Carlton Bioletti
- High altitude flying, by Paul B. King and Thomas Carroll
- Hydrodynamic tests in the N.A.C.A. tank of a model of the hull of the short Calcutta flying boat, by Kenneth E. Ward
- Internal-flow systems for aircraft, by F.M. Rogallo
- Damping characteristics of dashpots, by John B. Peterson
- Air flow investigation for location of angle of attack head on a JN4h airplane, by R.G. Freeman
- The aerodynamic analysis of the gyroplane rotating-wing system, by John B. Wheatley
- Determination of climbing ability, by H. Blasius
- The employment of airships for the transport of passengers: indications on the maximum limits of their useful load, distance covered, altitude and speed, Future of aerial transportation in public services, by Umberto Nobile
- Notes on longitudinal stability and balance, by E.P. Warner
- Estimation of moments of inertia of airplanes from design data, by H.W. Kirschbaum
- The optical wing aligning device of the Langley Field tunnel, by F.H. Norton and D.L. Bacon
- Effect of aileron displacement on wing characteristics, by R.H. Heald
- Compression tests of some 17S-T aluminum-alloy specimens of I cross section, by H.N. Hill
- Charts for calculating the performance of airplanes having constant-speed propellers, by Roland J. White and Victor J. Martin
- Extract from a report on the resistance of spheres of small diameter in an airstream of high velocity, by A. Toussaint and Lt. Hayer
- Influence of fuel-oil temperature on the combustion in a prechamber compression-ignition engine, by Harold C. Gerrish and Bruce E. Ayer
- Drag of exposed fittings and surface irregularities on airplane fuselages, by Donald H. Wood
- Amplitude of supersonic diffuser flow pulsations, by William H. Sterbentz and Joseph Davids
- The comparison of well-known and new wing sections tested in the variable density wind tunnel, by George J. Higgins
- The accuracy of the substitute-stringer approach for determining the bending frequencies of multistringer box beams, by William W. Davenport
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