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Technical reports / National Advisory Committee for Aeronautics

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Medientyp: Schriftenreihe; Monographische Schriftenreihe
Titel: Technical reports / National Advisory Committee for Aeronautics
Weitere Titel: Nebent.: Reports
Hauptsacht. teils: Report
Beteiligte: USA National Advisory Committee for Aeronautics
Erschienen: Washington, DC: Gov. Print. Off., 1915-1959
Erscheinungsverlauf: Nr. 1.1915 - 1392.1958(1959)
Erschienen in: Aeronautics
USA. National Advisory Committee for Aeronautics: Annual report of the National Advisory Committee for Aeronautics / Administrative report including Technical reports
Sprache: Englisch
Schlagwörter: Monografische Reihe
Entstehung:
Anmerkungen:
Bestand der SLUB: 1.1915(1916) - 7.1915(1916); 13.1917(1918) - 82.1919(1920); 111.1921(1923) - 209.1924(1925); 337.1930(1931) - 364.1930(1931); 441.1933(1934) - 611.1937(1938); 804.1945(1949) - 1157.1953(1955) ; unter Signatur: 19 4 05859 ; enthalten in: Aeronautics (bis 507) u. Annual report of the National Advisory Committee for Aeronautics, Administrative report including Technical reports (ab 508); 13-23, 111-122, 159-185: 2 Ex.
Nachweis der bibliograph. selbständig erschienenen Reports als Monographie
508.1936 - 644.1939 ; unter Signatur: 19 4 05859 ; Angeb. an 'Annual report of the National Advisory Committee for Aeronautics, Administrative report including Technical reports'

Weiterer Bestand der SLUB:

> Verlagsreihe

Eggers, Alfred J. [Verfasser:in]; Allen, H. Julian [Verfasser:in]; Neice, Stanford E. [Verfasser:in]
A comperative analysis of the performance of long range hypervelocity vehicles by Alfred J. Eggers; H. Julian Allen and Stanford E. Neice
Washington: Gov. Print. Off., 1959

Coles, Willard D. [Verfasser:in]; Callaghan, Edmund E. [Verfasser:in]
Full scale investigation of several jet engine noise reduction nozzles by Willard D. Coles and Edmund E. Callaghan
Washington, DC: Gov. Print. Off., 1959

Pinns, Murray L. [Sonstige Person, Familie und Körperschaft]
NACA research on slurry fuels by M. L. Pinns
Washington: Gov. Print. Off., 1959

Flügge-Lotz, Irmgard [Verfasser:in]; Taylor, Charles Fayette [Verfasser:in]; Lindberg, H. E. [Verfasser:in]
Investigation of a nonlinear control system by I. Flügge-Lotz; C. F. Taylor, and H. E. Lindberg
Washington: Gov. Print. Off., 1959

Gracey, William [Verfasser:in]
Measurement of static pressure on aircraft by William Gracey
Washington, DC: Gov. Print. Off., 1959

Spreiter, John R. [Verfasser:in]; Alksne, Alberta Y. [Verfasser:in]
Thin airfoil theory based on approximate solution of the transonic flow equation by John R. Spreiter and Alberta Y. Alksne
Washington, DC: Gov. Print. Off., 1959

Kelly, Mark W. [Verfasser:in]; Anderson, Seth B. [Verfasser:in]; Innis, Robert C. [Verfasser:in]
Blowling-type boundary-layer control as applied to the trailing-edge flaps of a 35° swept-wing airplane by Mark W. Kelly; Seth B. Anderson and Robert C. Innis
Washington, DC: Gov. Print. Off., 1959

Jorgensen, Leland H. [Verfasser:in]; Perkins, Edward W. [Verfasser:in]
Investigation of some wake vortex characteristics of an inclined ogivecylinder body at mach number 2 by Leland H. Jorgensen ans Edward W. Perkins
Washington, DC: Gov. Print. Off., 1959

Tower, Leonard K. [Verfasser:in]; Breitwieser, Roland [Verfasser:in]; Gammon, Benson E. [Verfasser:in]
Theoretical combustion performance of several high energy fuels for ramjet engines by Leonard K. Tower, Roland Breitwieser, and Benson E. Gammon
Washington, DC: Gov. Print. Off., 1959

Wright, Ray H. [Verfasser:in]; Ritchie, Virgil S. [Verfasser:in]; Pearson, Albin O. [Verfasser:in]
Characteristics of the langley 8-foot transonic tunnel with slotted test section by Ray H. Wright; Virgil S. Ritchie, and Albin O. Pearson
Washington: Gov. Print. Off., 1959

Wilts, Charles H. [Verfasser:in]
Incompressible flutter characteristics of representative aircraft wings by Charles H. Wilts
Washington: Gov. Print. Off., 1959

Decker, Raymond Frank [Verfasser:in]; Rowe, John P. [Verfasser:in]; Freeman, J. W. [Verfasser:in]
Boron and zirconium from crucibile refractories in a complex heat resistant alloy by R. F. Decker; John P. Rowe, and J. W. Freeman
Washington: Gov. Print. Off., 1959

Pinkel, I. Irving [Sonstige Person, Familie und Körperschaft]
Origin and prevention of crash fires in turbojet aircraft by I. Irving Pinkel
Washington, DC: Gov. Print. Off., 1959

Shufflebarger, C. C. [Verfasser:in]; Payne, Chester B. [Verfasser:in]; Cahen, George L. [Verfasser:in]
A correlation of results of a flight investigation with results of an analytical study of effects of wing flexibility on wing strains due to gusts by C. C. Shufflebarger, Chester B. Payne, and George L. Cahen
Washington, DC: Gov. Print. Off., 1959

May, Charles E. [Verfasser:in]
The mechanism of thermal gradient mass transfer in the sodium hydroxide nickel system by Charles E. May
Washington, DC: Gov. Print. Off., 1959

Cook, Woodrow L. [Verfasser:in]; Anderson, Seth B. [Verfasser:in]; Cooper, George E. [Verfasser:in]
Area suction boundary-layer control as applied to the trailing-edge flaps of a 35° swept-wing airplane by Woodrow L. Cook; Seth B. Anderson and George E. Cooper
Washington, DC: Gov. Print. Off., 1959

Hill, P. R. [Verfasser:in]
A method of computing the transient temperature of thick walls from arbitrary variation of adiabatic wall temperature and heat transfer coefficient by P. R. Hill
Washington, DC: Gov. Print. Off., 1959

Graves, Charles C. [Verfasser:in]; Grobman, Jack S. [Verfasser:in]
Theoretical analysis of total pressure loss airflow distribution for tubular turbojet combustors with constant annulus and liner cross sectional areas by Charles C. Graves and Jack S. Grobman
Washington, DC: Gov. Print. Off., 1959

Van Dyke, Milton [Verfasser:in]
The similarity rules for second order subsonic and supersonic flow by Milton D. Van Dyke
Washington, DC: Gov. Print. Off., 1959

Kurbjun, Max C. [Verfasser:in]; Vogeley, Arthur W. [Verfasser:in]
Measurements of free space oscillating pressures near propellers at flight mach numbers to 0.72 by Max C. Kurbjun and Arthur W. Vogeley
Washington, DC: Gov. Print. Off., 1959

Diederich, Franklin W. [Verfasser:in]
The response of an airplane to random atmospheric disturbances by Franklin W. Diederich
Washington, DC: Gov. Print. Off., 1959

Lassiter, Leslie W. [Verfasser:in]; Hess, Robert W. [Verfasser:in]
Calculated and measured stresses in simple panels subject to intense random acoustic loading including the near noise field of a turbojet engine by Leslie W. Lassiter and Robert W. Hess
Washington, DC: Gov. Print. Off., 1959

Jorgensen, Leland H. [Verfasser:in]
Elliptic cones alone and with wings at supersonic speeds by Leland H. Jorgensen
Washington, DC: Gov. Print. Off., 1959

Reshotko, Eli [Verfasser:in]; Beckwith, Ivan E. [Verfasser:in]
Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary prandtl number by Eli Reshotko and Ivan E. Beckwith
Washington, DC: Gov. Print. Off., 1959

Boatright, William B. [Verfasser:in]
An analysis of pressure studies and experimental and theoretical downwash and sidewash behind five pointed tip wings at supersonic speeds by William B. Boatright
Washington, DC: Gov. Print. Off., 1959

Allen, H. Julian [Verfasser:in]; Eggers, Alfred J. [Verfasser:in]
A study of the motion and aerodynamic heating of ballistic missiles entering the earth's atmosphere at high supersonic speeds by H. Julian Allen and A. J. Eggers
Washington: Gov. Print. Off., 1959

Drell, Isadore L. [Verfasser:in]; Belles, Frank E. [Verfasser:in]
Survey of hydrogen combustion properties by Isadore L. Drell and Frank E. Belles
Washington: Gov. Print. Off., 1959

Perkins, Edward W. [Verfasser:in]; Jorgensen, Leland H. [Verfasser:in]; Sommer, Simon C. [Verfasser:in]
Investigation of the drag of various axially symmetric noise shapes of fineness ratio 3 for mach numbers from 1.24 to 7.4 by Edward W. Perkins; Leland H. Jorgensen, and Simon C. Sommer
Washington, DC: Gov. Print. Off., 1959

Emery, James C. [Sonstige Person, Familie und Körperschaft]
Systematic two-dimensional cascade tests of NACA 65-series compressor blades at low speeds by James C. Emery
Washington, DC: Gov. Print. Off., 1959

Evans, Albert J. [Verfasser:in]; Liner, George [Verfasser:in]
A wind tunnel investigation of the aerodynamik characteristics of a full scale supersonic type three-blade propeller at mach numbers to 0.96 by Albert J. Evans and George Liner
Washington, DC: Gov. Print. Off., 1959

Eggers, Alfred J. [Verfasser:in]
A method for simulating the atmospheric entry of long range ballistic missils by A. J. Eggers
Washington: Gov. Print. Off., 1959

Stowell, Elbridge Z. [Verfasser:in]
A phenomenological relation between stress, strain rate, and temperature for metals at elevated temperatures by Elbridge Z. Stowell
Washington, DC: U.S. Gov. Print. Off., 1958

Doenhoff, Albert E. von [Verfasser:in] ; Horton, Elmer A. [Sonstige Person, Familie und Körperschaft]
A low-speed experimental investigation of the effect of a sandpaper type of roughness on boundary-layer transition by Albert E. von Doenhoff and Elmer A. Horton
Washington, DC: US Gov. Print. Off., 1958

Jonash, Edmund R. [Verfasser:in]; Wear, Jerrold D. [Verfasser:in]; Cook, William P. [Verfasser:in]
Effect of fuel variables on carbon formation in turbojet-engine combustors by Edmund R. Jonash, Jerrold D. Wear and William P. Cook
Washington, DC: US Gov. Print. Off., 1958

Cahn, Maurice S. [Verfasser:in]
An experimental investigation of sting support effects on drag and a comparsion with jet effects at transonic speeds by Maurice S. Cahn
Washington, DC: Gov. Print. Off., 1958

Barnett, Henry C. [Herausgeber:in]
Basic considerations in the combustion of hydrocarbon fuels with air ed. by Henry C. Barnett
Washington, DC: Gov. Print. Off., 1958

Brun, Rinaldo J. [Verfasser:in]
Cloud droplet ingestion in engine inlets with inlet velocity ratios of 1.0 and 0.7 by Rinaldo J. Brun
Washington, DC: Gov. Print. Off., 1958

Furlong, G. Chester [Verfasser:in]; MacHugh, James G. [Verfasser:in]
A summary and analysis of the low speed longitudinal characteristics of swept wings at the Reynolds number by G. Chester Furlong and James G. McHugh
Washington, DC: Gov. Print. Off., 1958

Blackshear, Perry L. [Verfasser:in]
Growth of disturbances in a flame-generated shear region by Perry L. Blackshear
Washington, DC: US Gov. Print. Off., 1958

Houbolt, John C. [Verfasser:in] ; Brooks, George W. [Sonstige Person, Familie und Körperschaft]
Differential equations of motion for combined flapwise bending, chordwise bending, and torsion of twisted nonuniform rotor blades by John C. Houbolt and George W. Brooks
Washington, DC: US Gov. Print. Off., 1958

Esgar, Jack B. [Verfasser:in]; Schum, Eugene F. [Verfasser:in]; Curren, Arthur N. [Verfasser:in]
Effect of chord size on weight and cooling characteristics of air-cooled turbine blades by Jack B. Esgar, Eugene F. Schum and Arthur N. Curren
Washington, DC: US Gov. Print. Off., 1958

A summary of preliminary investigations into the characteristics of combustion screech in ducted burners by Lewis Laboratory Staff
Washington, DC: US Gov. Print. Off., 1958

Heaslet, Maxwell A. [Verfasser:in] ; Fuller, Franklyn B. [Sonstige Person, Familie und Körperschaft]
Drag minimization for wings and bodies in supersonic flow by Max A. Heaslet and Franklyn B. Fuller
Washington, DC: US Gov. Print. Off., 1958

Chapman, Dean R. [Verfasser:in] ; Kuehn, Donald M. [Sonstige Person, Familie und Körperschaft]; Larson, Howard K. [Sonstige Person, Familie und Körperschaft]
Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition by Dean R. Chapman; Donald M. Kuehn; Howard K. Larson
Washington, DC: US Gov. Print. Off., 1958

Heldenfels, Richard R. [Verfasser:in]; Vosteen, Louis F. [Verfasser:in]
Approximate analysis of effects of large deflections and initial twist on torsional stiffness of a cantilever plate subjected to thermal stresses by Richard R. Heldenfels and Louis F. Vosteen
Washington, DC: US Gov. Print. Off., 1958

Sanders, J. Lyell [Verfasser:in] ; MacComb, Harvey G. [Sonstige Person, Familie und Körperschaft]; Schlechte, Floyd R. [Sonstige Person, Familie und Körperschaft]
A variational theorem for creep with apllications to plates and columns by J. Lyell Sanders, Harvey G. McComb and Floyd R. Schlechte
Washington, DC: U.S. Gov. Print. Off., 1958

Sternfield, Leonard [Verfasser:in]
A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver by Leonard Sternfield
Washington, DC: U.S. Gov. Print. Off., 1958

Gustafson, F. B. [Verfasser:in] ; Tapscott, Robert J. [Sonstige Person, Familie und Körperschaft]
Methods for obtaining desired helicopter stability characteristics and procedures for stability predictions by F. B. Gustafson and Robert J. Tapscott
Washington, DC: US Gov. Print. Off., 1958

Coleman, Robert P. [Verfasser:in]; Feingold, Arnold M. [Verfasser:in]
Theory of self-excited mechanical oscillations of helicopter rotors with hinged blades by Robert P. Coleman and Arnold M. Feingold
Washington, DC: US Gov. Print. Off., 1958

Shuford, Charles L. [Verfasser:in]
A theoretical and experimental study of planing surfaces including effects of cross section and plan form by Charles L. Shuford
Washington, DC: US Gov. Print. Off., 1958

Fisher, Lloyd J. [Verfasser:in]; Hoffman, Edward L. [Verfasser:in]
Ditching investigations of dynamic models and effects of design parameters on ditching characteristics by Lloyd J. Fisher and Edward L. Hoffman
Washington, DC: US Gov. Print. Off., 1958

Brown, B. Porter [Verfasser:in]
Ground simulator studies of the effects of valve friction, stick friction, flexibility, and backlash on power control system quality by B. Porter Brown
Washington, DC: US Gov. Print. Off., 1958

Bobbitt, Percy J. [Verfasser:in]
Linearzed lifting surface and lifting line evaluations of sidewash behind rolling triangular wings at supersonic speeds by Percy J. Bobbitt
Washington, DC: Gov. Print. Off., 1958

Pitts, William C. [Verfasser:in]; Nielsen, Jack N. [Verfasser:in]; Kaattari, George E. [Verfasser:in]
Lift and center of pressure of wing body tail combinations at subsonic, transonic, and supersonic speeds by William C. Pitts, Jack N. Nielsen and George E. Kaattari
Washington: Gov. Print. Off., 1958

Povolny, John H. [Verfasser:in]; Steffen, Fred W. [Verfasser:in]; MacArdle, Jack G. [Verfasser:in]
Summary of scale model thrust reverser investigation by John H. Povolny; Fred W. Steffen and Jack G. McArdle
Washington, DC: Gov. Print. Off., 1958

Heyson, Harry H. [Verfasser:in]; Katzoff, S. [Verfasser:in]
Induced velocities near a lifting rotor with nonuniform disk loading by Harry H. Heyson and S. Katzoff
Washington, DC: Gov. Print. Off., 1958

Fisher, Lewis R. [Verfasser:in]
Experimental determination of effects of frequency and amplitude on the lateral stability derivatives for a delta, a swept, and an unswept wing oscillating in yaw by Lewis R. Fisher
Washington, DC: US Gov. Print. Off., 1958

Rossow, Vernon J. [Verfasser:in]
On flow of electrically conducting fluids over a flat plate in the presence of a transverse magnetic field by Vernon J. Rossow
Washington, DC: US Gov. Print. Off., 1958

Johnson, R. D. [Verfasser:in]; Young, A. P. [Verfasser:in]; Schwope, A. D. [Verfasser:in]
Plastic deformation of aluminium single crystals at elevated temperatures by R. D. Johnson, A. P. Young and A. D. Schwope
Washington, DC: Gov. Print. Off., 1957

Rainey, Gerald [Verfasser:in]
Measurement of aerodynamic forces for various mean angles of attack on an airfoil oscillating in pitch and two finite-span wings oscillating in bending with emphasis on damping in the stall by Gerald Rainey
Washington, DC: Gov. Print. Off., 1957

Mathauser, Eldon E. [Verfasser:in]; Deveikis, William D. [Verfasser:in]
Investigation of the compressive strength and creep lifetime 2024-T3 aluminium-alloy plates at elevated temperatures by Eldon E. Mathauser and William D. Deveikis
Washington, DC: US Gov. Print. Off., 1957

Kline, G. M. [Sonstige Person, Familie und Körperschaft]
Development of craze and impact resistance in glazing plastics by multiaxial stretching by G. M. Kline
Washington, DC: Gov. Print. Off., 1957

Cooperative investigation of relationship between static and fatigue properties of wrought N-155 alloy at elevated temperatures by NACA subcommittee on power-plant materials
Washington, DC: Gov. Print. Off., 1957

Spreiter, John R. [Verfasser:in]; Sacks, Alvin H. [Verfasser:in]
A theoretical study of the aerodynamics of slender cruciform-wing arrangements and their wakes by John R. Spreiter and Alvin H. Sacks
Washington, DC: Gov. Print. Off., 1957

MacComb, Harvey G. [Verfasser:in]
Torsional stiffness of thin-walled shells having reinforced cores and rectangular, triangular, or diamond cross section by Harvey G. McComb jr
Washington, DC: US Gov. Print. Off., 1957

Philipps, William H. [Verfasser:in] ; Kuehnel, Helmut A. [Sonstige Person, Familie und Körperschaft]; Whitten, James B. [Sonstige Person, Familie und Körperschaft]; Phillips, William H. [Sonstige Person, Familie und Körperschaft]
Flight investigation of the effectiveness of an automatic aileron trim control device for personal airplanes by William H. Philipps, Helmut A. Kuehnel and James B. Whitten
Washington, DC: US Gov. Print. Off., 1957

Lomax, Harvard [Verfasser:in]; Heaslet, Maxwell A. [Verfasser:in]
A special method for finding body distortions that reduce the wave drag of wing and body combinations at supersonic speeds by Harvard Lomax and Max A. Heaslet
Washington, DC: Gov. Print. Off., 1957

MacCready, Robert R. [Verfasser:in]
Extrapolation techniques applied to matrix methods in neutron diffusion problems by Robert R. McCready
Washington, DC: Gov. Print. Off., 1957

Cohen, Clarence B. [Verfasser:in]; Reshotko, Eli [Verfasser:in]
The compressible laminar boundary layer with heat transfer and arbitary pressure gradient by Clarence B. Cohen and Eli Reshotko
Washington, DC: Gov. Print. Off., 1957

Laurence, James C. [Verfasser:in]
Intensity, scale, and spectra of turbulence in mixing region of free subsonic jet by James C. Laurence
Washington, DC: Gov. Print. Off., 1957

Cohen, Clarence B. [Verfasser:in]; Reshotko, Eli [Verfasser:in]
Similar solutions for the compressible laminar boundary layer with heat transfer and pressure gradient by Clarence B. Cohen and Eli Reshotko
Washington, DC: Gov. Print. Off., 1957

Lomax, Harvard [Verfasser:in]
Nonlifting wing-body combinations with certain geometric restraints having minimum wave drag at low supersonic speeds by Harvard Lomax
Washington, DC: US Gov. Print. Off., 1957

Skoog, Richard B. [Verfasser:in]
An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-wing airplane by Richard B. Skoog
Washington, DC: US Gov. Print. Off., 1957

Harder, Keith C. [Verfasser:in]; Klunker, E. B. [Verfasser:in]
On slender-body theory at transonic speeds by Keith C. Harder and E. B. Klunker
Washington, DC: US Gov. Print. Off., 1957

Heaslet, Maxwell A. [Verfasser:in] ; Spreiter, John R. [Sonstige Person, Familie und Körperschaft]
Three-dimensional transonic flow theory applied to slender wings and bodies by Max A. Heaslet and John R. Spreiter, Ames Aeronautical Laboratory Moffett Field, Calif
Washington, DC: US Government Printing Office, 1957

Lubarsky, Bernard [Verfasser:in]; Kaufman, Samuel J. [Verfasser:in]
Review of experimental investigations of liquid metal heat transfer by Bernard Lubarsky and Samuel J. Kaufman
Washington, DC: Gov. Print. Off., 1957

Grant, Frederick C. [Verfasser:in]
The proper combination of lift loadings for least drag on a supersonic wing by Frederick C. Grant
Washington, DC: Gov. Print. Off., 1957

Holzhauser, Curt A. [Verfasser:in]; Bray, Richard S. [Verfasser:in]
Wind tunnel and flight investigations of the use of leading edge area suction for the purpose of increasing the maximum lift coefficient of a 35 o swept wing airplane by Curt A. Holzhauser and Richard S. Bray
Washington, DC: Gov. Print. Off., 1957

Tucker, Maurice [Verfasser:in]
Interaction of a free flame front with a turbulence field by Maurice Tucker
Washington, DC: Gov. Print. Off., 1957

Cook, Francis E. [Verfasser:in]; Milwitzky, Benjamin [Verfasser:in]
Effect of interaction on landing gear behavior and dynamic loads in a flexible airplane structure by Francis E. Cook and Benjamin Milwitzky
Washington, DC: Gov. Print. Off., 1957

Nelson, Herbert C. [Verfasser:in]; Cunningham, Herbert J. [Verfasser:in]
Theoretical investigation of flutter of two dimensional flat panels with one surface exposed to supersonic potential flow by Herbert C. Nelson and Herbert J. Cunningham
Washington, DC: Gov. Print. Off., 1957

Sears, R. I. [Verfasser:in]; Merlet, C. F. [Verfasser:in]; Putland, L. W. [Verfasser:in]
Flight determination of drag of normal shock nose inlets with various cowling profiles at mach numbers from 0.9 to 1.5 by R. I. Sears, C. F. Merlet and L. W. Putland
Washington, DC: Gov. Print. Off., 1957

Press, Harry [Verfasser:in]; Meadows, May T. [Verfasser:in]; Hadlock, Ivan [Verfasser:in]
A reevaluation of data on atmospheric turbulence and airplane gust loads for application in spectral calculations by Harry Press, May T. Meadows and Ivan Hadlock
Washington, DC: Gov. Print. Off., 1957

Leonard, Robert W. [Verfasser:in]; Hedgepeth, John M. [Verfasser:in]
On panel flutter and divergence of infinitely unstiffened and ring-stiffened thin-walled circular cylinders by Robert W. Leonard and John M. Hedgepeth
Washington, DC: US Gov. Print. Off., 1957

Gracey, William [Verfasser:in]
Wind tunnel investigation of a number of total pressure tubes at high angeles of attack subsonic, transonic, and supersonic speeds by William Gracey
Washington, DC: Gov. Print. Off., 1957

Margolis, Kenneth [Verfasser:in]; Bobbitt, Percy J. [Verfasser:in]
Theoretical calculations of the pressures, forces, and moments at supersonic speeds due to various lateral motions acting on thin isolated vertical tails by Kenneth Margolis and Percy J. Bobbitt
Washington, DC: Gov. Print. Off., 1957

Eggers, A. J. [Sonstige Person, Familie und Körperschaft]; Resnikoff, Meyer M. [Sonstige Person, Familie und Körperschaft]; Dennis, David H. [Sonstige Person, Familie und Körperschaft]
Bodies of revolution having minimum drag at high supersonic airspeeds by A. J. Eggers
Washington, DC: US Gov. Print. Off., 1957

MacLellan, Charles H. [Verfasser:in] ; Bertram, Mitchel H. [Sonstige Person, Familie und Körperschaft]; Moore, John A. [Sonstige Person, Familie und Körperschaft]
An investigation of four wings of square plan forms at a Mach number of 6.9 in the Langley 11-inch hypersonic tunnel by Charles H. McLellan, Mitchel H. Bertram and John A. Moore
Washington, DC: US Gov. Print. Off., 1957

Moeckel, W. E. [Verfasser:in]
Some effects of bluntness on boundary layer transition and heat transfer at supersonic speeds by W. E. Moeckel
Washington, DC: Gov. Print. Off., 1957

Kramer, James J. [Verfasser:in]; Prian, Vasily D. [Verfasser:in]; Wu, Chung-Hua [Verfasser:in]
Theoretical analysis of incopressible flow through a radial-inlet centrifugal impeller at various weight flows by James J. Kramer, Vasily D. Prian and Chung-Hua Wu
Washington, DC: Gov. Print. Off., 1957

Moore, Franklin K. [Verfasser:in]
Lift hysteresis at stall as an unstead boundary layer phenomenon by Franklin K. Moore
Washington, DC: Gov. Print. Off., 1957

Smiley, Robert F. [Verfasser:in]
Correlation, evaluation, and extension of linearized theories for tire motion and wheel shimmy by Robert F. Smiley
Washington, DC: US Gov. Print. Off., 1957

Nothwang, George J. [Verfasser:in]
An evaluation of four experimental methods for measuring mean properties of a supersonic turbulent boundary layer by George J. Nothwang
Washington, DC: US Gov. Print. Off., 1957

Maynard, Julian D. [Verfasser:in]; Salters, Leland B. [Verfasser:in]
Aerodynamic characteristics at high speeds of related full-scale propellers having different blade-section cambers by Julian D. Maynard and Leland B. Salters
Washington, DC: US Gov. Print. Off., 1957

Alksne, Alberta Y. [Verfasser:in]
Determination of vortex paths by series expansion technique with application to cruciform wings by Alberta Y. Alksne
Washington, DC: US Gov. Print. Off., 1957

Jones, Robert T. [Verfasser:in]
Theory of wing body drag at supersonic speeds by Robert T. Jones
Washington, DC: Gov. Print. Off., 1957

Schubauer, Galen B. [Verfasser:in]; Klebanoff, P. S. [Verfasser:in]
Contributions on the mechanics of boundary layer transition by G. B. Schubauer and P. S. Klebanoff
Washington, DC: Gov. Print. Off., 1957

Rogallo, Vernon L. [Verfasser:in]; Yaggy, Paul F. [Verfasser:in]; MacCloud, John L. [Verfasser:in]
An analysis of once-per-revolution oscillating aerodynamic thrust loads on single-rotation propellers on tractor airplanes at zero yaw by Vernon L. Rogallo, Paul F. Yaggy and John L. McCloud
Washington, DC: Gov. Print. Off., 1957

Bertram, Mitchel H. [Verfasser:in]
Exploratory investigation of boundary-layer transition on a hollow cylinder at a Mach number of 6.9 by Mitchel H. Bertram
Washington, DC: US Gov. Print. Off., 1957

Curfman, Howard J. [Verfasser:in]
Theoretical and analog studies of the effects of nonlinear stability derivatives on the longitudinal motions of an aircraft in response to step control deflections and to the influence of proportional automatic control by Howard J. Curfman
Washington, DC: US Gov. Print. Off., 1956

Klebanoff, P. S. [Verfasser:in]
Characteristics of turbulence in a boundary layer with zero pressure gradient by P. S. Klebanoff
Washington, DC: Gov. Print. Off., 1956

Bisson, Edmond E. [Sonstige Person, Familie und Körperschaft]
Friction, wear, and surface damage of metals as affected by solid surface films by Edmond E. Bisson
Washington, DC: Gov. Print. Off., 1956

Trimpi, Robert L. [Verfasser:in]
A theory for stability and Buzz pulsation amplitude in ram jets and an experimental investigation including scale effects by Robert L. Trimpi
Washington, DC: US Gov. Print. Off., 1956

Corrsin, Stanley [Verfasser:in]; Kistler, Alan L. [Verfasser:in]
Free stream boundaries of turbulent flows by Stanley Corrsin and Alan L. Kistler
Washington, DC: Gov. Print. Off., 1956

MacComb, Harvey G. [Verfasser:in]
Stress analysis of circular semimonocoque cylinders with cutouts by Harvey G. McComb
Washington, DC: Gov. Print. Off., 1956

Wright, Ray H. [Verfasser:in]; Ward, Vernon G. [Verfasser:in]
NACA transonic wind tunnel test sections by Ray H. Wright and Vernon G. Ward
Washington, DC: Gov. Print. Off., 1956

Standard atmosphere - tables and data for altitudes to 65,800 feet International Civil Aviation Organization
Washington, DC: Gov. Print. Off., 1956

Furlong, G. Chester [Verfasser:in]; Bollech, Thomas V. [Verfasser:in]
Effect of ground interference on the aerodynamic and flow characteristics of a 42° sweptback wing at reynolds number up to 6.8 x 10 6 by G. Chester Furlong and Thomas V. Bollech
Washington, DC: Gov. Print. Off., 1956

Eckert, Ernst R. G. [Verfasser:in]; Livingood, John N. B. [Verfasser:in]
Calculations of laminar heat transfer aroung cylinders of arbitary cross section and transpiration cooled walls with application to turbine blade cooling by E. R. G. Eckert and J. N. B. Livingood
Washington, DC: Gov. Print. Off., 1956

Donegan, James J. [Verfasser:in]; Robinson, Samuel W. [Verfasser:in]; Gates, Ordway B. [Verfasser:in]
Determination of lateral stability derivatives and transfer function coefficients from frequency response data for lateral motions by James J. Donegan, Samuel W. Robinson and Ordway B.Gates
Washington, DC: Gov. Print. Off., 1956

Brun, R. J. [Sonstige Person, Familie und Körperschaft]
Impingement of cloud droplets on a cylinder and procedure for measuring liquid water content and droplet sizes in supercooled clouds by rotating multicylinder method by R. J. Brun
Washington, DC: Gov. Print. Off., 1956

Amer, Kenneth B. [Verfasser:in]; Gessow, Alfred [Verfasser:in]
Charts for estimating tail rotor contribution to helicopter directional stability and control in low speed flight by Kenneth B. Amer and Alfred Gessow
Washington, DC: Gov. Print. Off., 1956

Spreiter, John R. [Verfasser:in]; Alksne, Alberta Y. [Verfasser:in]
Theoretical prediction of pressure distributions on nonlifting airfoils at high subsonic speeds by John R. Spreiter and Alberta Alksne
Washington, DC: Gov. Print. Off., 1956

Seiff, Alvin [Verfasser:in]
A free flight wind tunnel for aerodynamic testing at hypersonic speeds by Alvin Seiff
Washington, DC: Gov. Print. Off., 1956

Goodman, Alex [Verfasser:in]; Thomas, David F. [Verfasser:in]
Effects of wing position and fuselage size on the low speed static and rolling stability characteristics of a delta wing model by Alex Goodman and David F. Thomas
Washington, DC: Gov. Print. Off., 1956

Lietzke, A. F. [Verfasser:in]
Theoretical and experimental investigation of heat transfer by laminar natural convection between parallel plates by A. F. Lietzke
Washington, DC: Gov. Print. Off., 1956

Huston, Wilber B. [Verfasser:in]; Skopinski, T. H. [Verfasser:in]
Measurement and analysis of wing and tail buffeting loads on a fighter airplane by Wilber B. Huston and T. H. Skopinski
Washington, DC: Gov. Print. Off., 1956

Matthews, Clarence W. [Verfasser:in]
Theoretical study of the tunnel boundary lift interference due to slotted walls in the presence of the trailing-vortex system of a lifting model by Clarence W. Matthews
Washington, DC: Gov. Print. Off., 1956

Czarnecki, K. R. [Verfasser:in]; Sinclair, Archibald R. [Verfasser:in]
An investigation of the effects of heat transfer on boundary layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61 by K. R. Czarnecki and Archibald R. Sinclair
Washington, DC: US Gov. Print. Off., 1956

Towe, George C. [Verfasser:in]; Gomberg, Henry J. [Verfasser:in]; Freeman, J. W. [Verfasser:in]
High resolution autoradiography by George C. Towe, Henry J. Gomberg, and J. W. Freeman
Washington, DC: US Gov. Print. Off., 1956

Semonian, Joseph W. [Verfasser:in]; Peterson, James P. [Verfasser:in]
An analysis of the stability and ultimate compressive strength of short sheet stringer panels with special reference to the influence of the riveted connection between sheet and stringer by Joseph W. Semonian and James P. Peterson
Washington, DC: Gov. Print. Off., 1956

Watkins, Charles E. [Verfasser:in]; Berman, Julian H. [Verfasser:in]
On the kernel function of the integral equation relating the lift and downwash distributions of oscillating wings in subsonic flow by Charles E. Watkins and Julian H. Berman
Washington, DC: US Gov. Print. Off., 1956

Chapman, Dean R. [Verfasser:in]
Some possibilities of using gas mixtures other than air in aerodynamic research by Dean R. Chapman
Washington, DC: US Gov. Print. Off., 1956

Tucker, Warren A. [Verfasser:in]
A method for the design of sweptback wings warped to produce specified flight characteristics at supersonic speeds by Warren A. Tucker
Washington, DC: Gov. Print. Off., 1956

Watkins, Charles E. [Verfasser:in]; Runyan, Harry L. [Verfasser:in]; Woolston, Donald S. [Verfasser:in]
On the kernel function of the integral equation relating the lift and downwash distributions of oscillating finite wings in subsonic flow by Charles E. Watkins; Harry L. Runyan and Donald S. Woolston
Washington, DC: Gov. Print. Off., 1956

Queijo, M. J. [Verfasser:in]
Theoretical span load distributions and rolling moments for sideslipping wings of arbitrary plan form in incompressible flow by M. J. Queijo
Washington, DC: US Gov. Print. Off., 1956

Harder, Keith C. [Verfasser:in]; Rennemann, Conrad [Verfasser:in]
On boattail bodies of revolution having minimum wave drag by Keith C. Harder and Conrad Rennemann
Washington, DC: US Gov. Print. Off., 1956

Whitcomb, Richard T. [Verfasser:in]
A study of the zero-lift drag-rise characteristics of wing-body combinations near the speed of sound by Richard T. Whitcomb
Washington, DC: US Gov. Print. Off., 1956

Anderson, Seth B. [Verfasser:in]; Bray, Richard S. [Verfasser:in]
A flight evaluation of the longitudinal stability characteristics associated with the pitch up of a swept-wing airplane in maneuvering flight at transonic speeds by Seth B. Anderson and Richard S. Bray
Washington, DC: US Gov. Print. Off., 1956

Van Dyke, Milton [Verfasser:in]
Second-order subsonic airfoil theory including edge effects by Milton D. van Dyke
Washington, DC: US Gov. Print. Off., 1956

Milwitzky, Benjamin [Verfasser:in]; Lindquist, Dean C. [Verfasser:in]; Potter, Dexter M. [Verfasser:in]
An experimental study of applied ground loads in landing by Benjamin Milwitzky, Dean C. Lindquist, and Dexter M. Potter
Washington, DC: Gov. Print. Off., 1956

Eggers, Alfred J. [Verfasser:in]; Savin, Raymond C. [Verfasser:in]
A unified two-dimensional approach to the calculation of three-dimensional hypersonic flows, with application to bodies of revolution by A. J. Eggers and Raymond C. Savin
Washington, DC: Gov. Print. Off., 1956

Nielsen, Jack N. [Verfasser:in]
Quasi-cylindrical theory of wing body interference at supersonic speeds and comparison with experiment by Jack N. Nielsen
Washington, DC: Gov. Print. Off., 1956

Beam, Benjamin H. [Verfasser:in]
A wind-tunnel test technique for measuring the dynamic rotary stability derivatives at subsonic and supersonic speeds by Benjamin H. Beam
Washington, DC: US Gov. Print. Off., 1956

Lassiter, Leslie W. [Verfasser:in]; Hubbard, Harvey H. [Verfasser:in]
The near noise field of static jets and some model studies of devices for noise reduction by Leslie W. Lassiter and Harvey H. Hubbard
Washington, DC: U.S. Gov. Print. Off., 1956

Runyan, Harry L. [Verfasser:in] ; Woolston, Donald S. [Sonstige Person, Familie und Körperschaft]; Rainey, A. Gerald [Sonstige Person, Familie und Körperschaft]
Theoretical and experimental investigation of the effect of tunnel walls on the forces on an oscillating airfoil in two-dimensional subsonic compressible flow by Harry L. Runyan, Donald S. Woolston and A. Gerald Rainey
Washington, DC: U.S. Gov. Print. Off., 1956

Kuhn, Richard E. [Verfasser:in] ; Draper, John William [Sonstige Person, Familie und Körperschaft]
Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 [degree] by Richard E. Kuhn and John W. Draper
Washington, DC: U.S. Gov. Print. Off., 1956

Gessow, Alfred [Verfasser:in] ; Tapscott, Robert J. [Sonstige Person, Familie und Körperschaft]
Charts for estimating performance of high-performance helicopters by Alfred Gessow
Washington, DC: US Gov. Print. Off., 1956

Potter, Andrew E. [Verfasser:in]; Berlad, A. L. [Verfasser:in]
A thermal equation for flame quenching by A. E. Potter and A. L. Berlad
Washington, DC: Gov. Print. Off., 1956

Morduchow, Morris [Verfasser:in]
Analysis and calculation by integral methods of laminar compressible boundary layer with heat transfer and with and without pressure gradient by Morris Morduchow
Washington, DC: Gov. Print. Off., 1956

Tolefson, H. B. [Verfasser:in]
Summary of derived gust velocities obtained from measurements within thunderstorms by H. B. Tolefson
Washington, DC: US Gov. Print. Off., 1956

Mickelsen, William R. [Verfasser:in]; Ernstein, Norman E. [Verfasser:in]
Propagation of a free flame in a turbulent gas stream by William R. Mickelsen and Norman E. Ernstein
Washington, DC: US Gov. Print. Off., 1956

Diederich, Franklin W. [Verfasser:in]; Zlotnick, Martin [Verfasser:in]
Calculated spanwise lift distributions, influence functions, and influence coefficients for unswept wings in subsonic flow by Franklin W. Diederich and Martin Zlotnick
Washington, DC: Gov. Print. Off., 1956

Lomax, Harvard [Verfasser:in]; Fuller, Franklyn B. [Verfasser:in]; Sluder, Loma [Verfasser:in]
Generalized indicial forces on deforming rectangular wings in supersonic flight by Harvard Lomax; Franklyn B. Fuller and Loma Sluder
Washington, DC: Gov. Print. Off., 1956

Wadlin, Kenneth L. [Verfasser:in]; Shuford, Charles L. [Verfasser:in]; MacGehee, John R. [Verfasser:in]
A theoretical and experimental investigation of the lift and drag characteristics of hydrofoils at subcritical and supercritical speeds by Kenneth L. Wadlin, Charles L. Shuford, and John R. McGehee
Washington, DC: Gov. Print. Off., 1956

Ribner, Herbert S. [Verfasser:in]
Shock turbulence interaction and the generation of noise by H. S. Ribner
Washington, DC: Gov. Print. Off., 1956

Friedman, Morris D. [Verfasser:in]; Cohen, Doris [Verfasser:in]
Arrangement of fusiform bodies to reduce the wave drag at supersonic speeds by Morris D. Friedman and Doris Cohen
Washington, DC: Gov. Print. Off., 1956

Love, Eugene S. [Verfasser:in]
Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles by Eugene S. Love
Washington, DC: US Gov. Print. Off., 1956

O'Bryan, Thomas C. [Verfasser:in]; Danforth, Edward C. B. [Verfasser:in]; Johnston, J. Ford [Verfasser:in]
Error in airspeed measurement due to the static pressure field ahead of an airplane at transonic speeds by Thomas C. O'Bryan, Edward C. B. Danforth, and J. Ford Johnston
Washington, DC: US Gov. Print. Off., 1956

Heaslet, Maxwell A. [Verfasser:in] ; Fuller, Franklyn B. [Sonstige Person, Familie und Körperschaft]
Axially symmetric shapes with minimum wave drag by Max A. Heaslet and Franklyn B. Fuller
Washington, D.C.: U.S. Gov. Print. Off., 1956

Tapscott, Robert J. [Verfasser:in] ; Amer, Kenneth B. [Sonstige Person, Familie und Körperschaft]
Studies of the speed stability of a tandem helicopter in forward flight by Robert J. Tapscott and Kenneth B. Amer
Washington, DC: U.S. Gov. Print. Off., 1956

MacDevitt, John B. [Verfasser:in]
A correlation by means of transonic similarity rules of experimentally determined characteristics of a series of symmetrical and cambered wings of rectangular plan form by John B. McDevitt
Washington, DC: Gov. Print. Off., 1956

Gallagher, James J. [Verfasser:in]; Mueller, James N. [Verfasser:in]
An investigation of the maximum lift of wings at supersonic speeds by James J. Gallagher and James N. Mueller
Washington, DC: Gov. Print. Off., 1956

Donoughe, Patrick L. [Verfasser:in]; Livingood, John N. B. [Verfasser:in]
Exact solutions of laminar boundary layer equations with constant property values for porous wall with variable temperature by Patrick L. Donoughe and John N. B. Livingood
Washington, DC: Gov. Print. Off., 1956

Wadlin, Kenneth L. [Verfasser:in]; Ramsen, John A. [Verfasser:in]; Vaughan, Victor L. [Verfasser:in]
The hydrodynamic characteristics of modified rectangular flat plates having aspect ratios of 1.00, 025, and 0.125 and operating near a water surface by Kenneth L. Wadlin, John A. Ramsen and Victor L. Vaughan
Washington, DC: US. Gov. Print. Off., 1955

Eckert, Ernst R. G. [Verfasser:in]; Diaguila, Anthony J. [Verfasser:in]
Experimental investigation of free convection heat transfer in vertical tube at large grashof numbers by E. R. G. Eckert and A. J. Diaguila
Washington, DC: Gov. Print. Off., 1955

Pack, George J. [Verfasser:in]; Phillips, W. E. [Verfasser:in]
Analog study of interacting and non-interacting multiple-loop control systems for turbojet engines by George J. Pack and W. E. Phillips
Washington, DC: US Gov. Print. Off., 1955

Deissler, Robert G. [Verfasser:in]
Analysis of turbulent heat transfer, mass transfer, and friction in smooth tubes at high Prandtl and Schmidt numbers by Robert G. Deissler
Washington, DC: Gov. Print. Off., 1955

Parker, Hermon M. [Verfasser:in]
Minimum drag ducted and pointed bodies of revolution based on linearized supersonic theory by Hermon M. Parker
Washington, DC: Gov. Print. Off., 1955

Silsby, Norman S. [Verfasser:in]
Statistical measurements of contact conditions of 478 transport-airplane landings during routine daytime operations by Norman S. Silsby
Washington, DC: US Gov. Print. Off., 1955

Osgood, William R. [Verfasser:in]
Column strength of tubes elastically restrained against rotation at the ends by William R. Osgood
Washington, DC: Gov. Print. Off., 1955

Abbott, Ira H. [Verfasser:in]; Doenhoff, Albert E. von [Verfasser:in]; Stivers, Louis S. [Verfasser:in]
Summary of airfoil data by Ira H. Abbott, Albert E. von Doenhoff and Louis S. Stivers
Washington, DC: National Advisory Committee for Aeronautics, 1945

Wenzinger, Carl J. [Verfasser:in]; Harris, Thomas A. [Verfasser:in]
Wind tunnel investigation of an NACA 23012 airfoil with various arrangements of slotted flaps by Carl J. Wenzinger and Thomas A. Harris
Washington, DC: Gov. Print. Off., 1939

Aitchison, Clyde S. [Verfasser:in]; Tuckerman, Louis B. [Verfasser:in]
The "Pack" method for compressive tests of thin specimens of materials used in thin-wall structures by C. S. Aitchison and L. B. Tuckerman
Washington, DC: Gov. Print. Off., 1939

Bicknell, Joseph [Verfasser:in]
Determination of the profile drag of an airplane wing in flight at high reynolds numbers by Joseph Bicknell
Washington, DC: Gov. Print. Off., 1939

Seidman, Oscar [Verfasser:in]; Neihouse, Anshal I. [Verfasser:in]
Free spinning wind tunnel tests of a low wing monoplane with systematic changes in wings and tails 4 Effect of center of gravity location by Oscar Seidman and A. I. Neihouse
[Washington, DC]: NACA, 1939

Silverstein, Abe [Verfasser:in]; Joyner, Upshur T. [Verfasser:in]
Experimental verification of the theory of oscillating airfoils by Abe Silverstein and Upshur T. Joyner
Washington, DC: Gov. Print. Off., 1939

Soulé, Hartley A. [Verfasser:in]; Gracey, William [Verfasser:in]
A flight comparison of conventional ailerons on a recetangular wing and of conventional and floating wing-tip on a tapered wing by H. A. Soulé and W. Gracey
Washington, DC: Gov. Print. Off., 1939

Silverstein, Abe [Verfasser:in]; Katzoff, S. [Verfasser:in]
Design charts for predicting downwash angles and wake characteristics behind plain and flapped wings by Abe Silverstein and S. Katzoff
Washington, DC: Gov. Print. Off., 1939

Schubauer, Galen B. [Verfasser:in]
Air flow in the boundary layer of an elliptic cylinder by G. B. Schubauer
Washington, DC: Gov. Print. Off., 1939

Rothrock, A. M. [Verfasser:in]; Spencer, R. C. [Verfasser:in]
The influence of directed air flow on combustion in a spark ignition engine by A. M. Rothrock and R. C. Spencer
Washington, DC: Gov. Print. Off., 1939

Silverstein, Abe [Verfasser:in]; Becker, John V. [Verfasser:in]
Determination of boundary layer transition on three symmetrical airfoils in the NACA full scale wind tunnel by Abe Silverstein and John V. Becker
Washington, DC: Gov. Print. Off., 1939

Brevoort, Maurice J. [Verfasser:in]; Joyner, Upshur T. [Verfasser:in]
Cooling on the front of an air cooled engine cylinder in a conventional engine cowling by M. J. Brevoort and U. T. Joyner
Washington, DC: Gov. Print. Off., 1939

Goett, Harry J. [Verfasser:in]; Reeder, J. P. [Verfasser:in]
Effects of elevator nose shape, gap, balance, and tabs on the aerodynamic characteristics of a horizontral tail surface by Harry J. Goett and J. P. Reeder
Washington, DC: Gov. Print. Off., 1939

Ellerbrock, Herman H. [Verfasser:in]; Biermann, Arnold E. [Verfasser:in]
Surface heat transfer coefficients of finned cylinders by Herman H. Ellerbrock and Arnold E. Biermann
Washington, DC: Gov. Print. Off., 1939

Schey, Oscar W. [Verfasser:in]; Pinkel, Benjamin [Verfasser:in]; Ellerbrock, Herman H. [Verfasser:in]
Correction of temperatures of air cooled engine cylinders for variation in engine and cooling conditions by Oscar W. Schey, Benjamin Pinkel and Hermann H. Ellerbrock
Washington, DC: Gov. Print. Off., 1938

Wenzinger, Carl J. [Verfasser:in]; Delano, James B. [Verfasser:in]
Pressure distribution over an NACA 23012 airfoil with a slotted and a plain flap by Carl J. Wenzinger and James B. Delano
Washington, DC: Gov. Print. Off., 1938

Jones, Robert T. [Verfasser:in]
The influence of lateral stability on disturbed motions of an airplane with special reference to the motions produced by gusts by Robert T. Jones
Washington, DC: Gov. Print. Off., 1938

Rothrock, A. M. [Verfasser:in]; Spencer, R. C. [Verfasser:in]
A photographic study of combustion and knock in a spark ignition engine by A. M. Rothrock and R. C. Spencer
Washington, DC: Gov. Print. Off., 1938

Garrick, Isadore E. [Verfasser:in]
On some reciprocal relations in the theory of nonstationary flows by I. E. Garrick
Washington, DC: Gov. Print. Off., 1938

Allen, Julian H. [Verfasser:in]
Calculation of the chordwise load distribution over airfoil sections with plain, split, or serially hinged trailing edge flaps by H. Julian Allen
Washington, DC: Gov. Print. Off., 1938

Hartman, Edwin P. [Verfasser:in]; Biermann, David [Verfasser:in]
The aerodynamic characteristics of full scale propellers having 2, 3, and 4 blades of clark y and RAF 6 airfoil sections by Edwin P. Hartmann and David Biermann
Washington, DC: Gov. Print. Off., 1938

Pearson, Henry A. [Verfasser:in]; Jones, Robert T. [Verfasser:in]
Theoretical stability and control characteristics of wings with various amounts of taper and twist by Henry A. Pearson and Robert T. Jones
Washington, DC: US Gov. Print. Off., 1938

Platt, Robert C. [Verfasser:in]
Aerodynamic characteristics of a wing [with fowler flaps] including flap loads, downwash, and calculated effect on take-off by Robert C. Platt
[Washington, DC]: US Gov. Print. Off., 1935

Biermann, David [Verfasser:in]; Herrnstein, William H. [Verfasser:in]
The interference between struts in various combinations by David Biermann and William H. Herrnstein
Washington, DC: NACA, 1933

Gelalles, A. G. [Verfasser:in]
Effect of orifice length diameter ration on fuel sprays for compression ignition engines by A. G. Gelalles
Washington, DC: US Gov. Print. Off., 1932

Wheatley, John B. [Verfasser:in]
Lift and drag characteristics and gliding performance of an autogiro as determined in flight by John B. Wheatley
Washington, DC: US Gov. Print. Off., 1932

MacAvoy, William H. [Verfasser:in]; Schey, Oscar W. [Verfasser:in]; Young, Alfred W. [Verfasser:in]
The effect on airplane performance of the factors that must be considered in applying low drag cowling to radial engines by William H. MacAvoy; Oscar W. Schey and Alfred W. Young
Washington, DC: US Gov. Print. Off., 1932

Weick, Fred E. [Verfasser:in]
Preliminary investigation of modifications to conventional airplanes to give nonstalling and short landing characteristics by Fred E. Weick
Washington, DC: US Gov. Print. Off., 1932

Weick, Fred E. [Verfasser:in] ; Wenzinger, Carl J. [Sonstige Person, Familie und Körperschaft]
Wind-tunnel research comparing lateral control devices, particularly at high angles of attack 1 Ordinary ailerons on rectangular wings / by Fred E. Weick and Carl J. Wenzinger
Washington, D.C.: US Gov. Print. Off., 1932

Schey, Oscar W. [Verfasser:in]
The comparative performance of superchargers by Oscar W. Schey
Washington, DC: US Gov. Print. Off., 1931

Freeman, Hugh B. [Verfasser:in]
The effect of small angles of yaw and pitch on the characteristics of airplane propellerss by Hugh B. Freeman
Washington, DC: US Gov. Print. Off., 1931

Theodorsen, Theodore [Verfasser:in]
A new principle of sound frequency analysis by Theodore Theodorsen
Washington, DC: US Gov. Print. Off., 1931

Dearborn, Clinton H. [Verfasser:in]; Kirschbaum, H. W. [Verfasser:in]
Maneuverability investigation of the F6C-3 airplane with special flight instruments by C. H. Dearborn and H. W. Kirschbaum
Washington, DC: US Gov. Print. Off., 1931

Darnell, T. H. [Verfasser:in]
The automotive ignition coil by T. H. Darnell
Washington, DC: US Gov. Print. Off., 1931

Soulé, Hartley A. [Verfasser:in]; Scudder, Nathan F. [Verfasser:in]
A method of flight measurement of spins by Hartley A. Soulé and Nathan F. Scudder
Washington, DC: US Gov. Print. Off., 1931

Knight, Montgomery [Verfasser:in]; Wenzinger, Carl J. [Verfasser:in]
Rolling moments due to rolling and yaw for four wing models in rotation by Montgomery Knight and Carl J. Wenzinger
Washington, DC: US Gov. Print. Off., 1931

Peck, William C. [Verfasser:in]; Besard, Albert P. [Verfasser:in]
Static, drop, and flight tests on Musselman type airwheels by William C. Peck and Albert P. Besard
Washington, DC: US Gov. Print. Off., 1931

Trayer, George W. [Verfasser:in]; March, H. W. [Verfasser:in]
Elastic instability of members having sections common in aircraft construction by George W. Trayer and H. W. March
Washington, DC: US Gov. Print. Off., 1931

Dearborn, Clinton H. [Verfasser:in]; Kirschbaum, H. W. [Verfasser:in]
Maneuverability investigation of an F6C-4 fighting airplane by C. H. Dearborn and H. W. Kirschbaum
Washington, DC: US Gov. Print. Off., 1931

Wenzinger, Carl J. [Verfasser:in]; Harris, Thomas A. [Verfasser:in]
The vertical wind tunnel of the national advisory committee for aeronautics by Carl J. Wenzinger and Thomas A. Harris
Washington, DC: US Gov. Print. Off., 1931

Schey, Oscar W. [Verfasser:in]; Biermann, Arnold E. [Verfasser:in]
The effect of valve timing upon the performance of a supercharged engine at altitude and an unsupercharged engine at sea level by Oscar W. Schey and Arnold E. Biermann
Washington, DC: US Gov. Print. Off., 1931

Rothrock, A. M. [Verfasser:in]
Combustion in a high speed compression ignition engine by A. M. Rothrock
Washington, DC: US Gov. Print. Off., 1931

Present status of aircraft instruments
Washington, DC: US Gov. Print. Off., 1931

Theodorsen, Theodore [Verfasser:in]
Investigation of the diaphragm type pressure cell by Theodore Theodorsen
Washington, DC: US Gov. Print. Off., 1931

Rhode, Richard V. [Verfasser:in]; Lundquist, Eugene E. [Verfasser:in]
Pressure distribution over the fuselage of a PW-9 pursuit airplane in flight by Richard V. Rhode and Eugene E. Lundquist
Washington, DC: US Gov. Print. Off., 1931

Trayer, George W. [Verfasser:in]; March, H. W. [Verfasser:in]
The torsion of members having sections common in aircraft construction by George W. Trayer and H. W. March
Washington, DC: US Gov. Print. Off., 1930

Brombacher, William G. [Verfasser:in]; Cordero, F. [Verfasser:in]
Pressure element of constant logarithmic stiffness for temperature compensated altimeter by W. G. Brombacher and F. Cordero
Washington, DC: US Gov. Print. Off., 1929

Schey, Oscar W. [Verfasser:in]; Biermann, Arnold E. [Verfasser:in]
The effect of cowling on cylinder temperatures and performance of a Wright J-5 engine by Oscar W. Schey and Arnold E. Biermann
Washington, DC: US Gov. Print. Off., 1929

Franklin, W. S. [Sonstige Person, Familie und Körperschaft]; Stillman, M. H. [Sonstige Person, Familie und Körperschaft]; Sanford, Raymond L. [Sonstige Person, Familie und Körperschaft]
Direction instruments in four parts
Washington, DC: Gov. Print. Off., [1929?]

Smith, Richard H. [Verfasser:in]
Aerodynamic theory and test of strut forms 1 by R. H. Smith
Washington, DC: US Gov. Print. Off., 1929

Aerodynamic characteristics of aerofoils 2 Continuation of report no. 93
Washington, DC: Gov. Print. Off., 1928

Mears, Atherton H. [Sonstige Person, Familie und Körperschaft]; Henrickson, H. B. [Sonstige Person, Familie und Körperschaft]; Brombacher, William G. [Sonstige Person, Familie und Körperschaft]; Peterson, John B. [Sonstige Person, Familie und Körperschaft]; Freeman, John R. [Sonstige Person, Familie und Körperschaft]
Altitude instruments in four parts
Washington, DC: Gov. Print. Off., [1922]

Hunt, Franklin L. [Verfasser:in]
Recent developments and outstanding problems by F. L. Hunt
Washington, DC: Gov. Print. Off., 1922

Hunt, Franklin L. [Sonstige Person, Familie und Körperschaft]; Stearns, H. O. [Sonstige Person, Familie und Körperschaft]
Aircraft speed instruments in three parts by F. L. Hunt and H. O. Stearns
Washington, DC: Gov. Print. Off., [1922?]

Washburn, G. E. [Sonstige Person, Familie und Körperschaft]; Sylvander, R. C. [Sonstige Person, Familie und Körperschaft]
Power plant instruments in five parts
Washington, DC: Gov. Print. Off., [1922?]

Hunt, Franklin L. [Verfasser:in]
Oxygen instruments by F. L. Hunt
Washington, DC: Gov. Print. Off., [1922]

Eaton, Herbert N. [Verfasser:in]
Aerial navigation and navigating instruments by H. N. Eaton
Washington, DC: Gov. Print. Off., [1922]

Parsons, Samuel Reynolds [Verfasser:in]
Turbulence in the air tubes of radiators for aircraft engines by S. R. Parsons
Washington, DC: Gov. Print. Off., 1921

Dickinson, H. C. [Verfasser:in]; Newell, F. B. [Verfasser:in]
A high speed engine pressure indicator of the balanced diaphragm type by H. C. Dickinson and F. B. Newell
Washington, DC: Gov. Print. Off., 1921

Durand, William Frederick [Sonstige Person, Familie und Körperschaft]; Lesley, E. P. [Sonstige Person, Familie und Körperschaft]
Experimental research on air propellers 4 By W. F. Durand and E. P. Lesley
Washington, DC: Gov. Print. Off., 1921

Hersey, Mayo D. [Verfasser:in]; Hunt, Franklin L. [Verfasser:in]; Eaton, Herbert N. [Verfasser:in]
The altitude effect on air speed indicators in two parts by Mayo D. Hersey, Franklin L. Hunt, and Herbert N. Eaton
Washington, DC: Gov. Print. Off., 1921

Kemble, E. C. [Verfasser:in]
The calculated performance of airplanes equipped with supercharging engines in two parts by E. C. Kemble
Washington, DC: Gov. Print. Off., 1921

Silsbee, Francis B. [Verfasser:in]
Simplified theory of the magneto by F. B. Silsbee
Washington, DC: Gov. Print. Off., [1921]

Hersey, Mayo D. [Verfasser:in]
General classification of instruments and problems including bibliography by Mayo D. Hersey
Washington, DC: Gov. Print. Off., [1921?]

Gage, Victor R. [Verfasser:in]
Some factors of airplane engine performance by Victor R. Gage
Washington, DC: Gov. Print. Off., 1921

Elmendorf, Armin [Verfasser:in]
Data on the design of plywood for aircraft by Armin Elmendorf
Washington, DC: Gov. Print. Off., [ca. 1920]

Parsons, Samuel Reynolds [Verfasser:in]; Kleinschmidt, R. V. [Verfasser:in]
Effects of nature of cooling surface on radiator performance by S. R. Parsons and R. V. Kleinschmidt
Washington, DC: Gov. Print. Off., 1920

Dickinson, H. C. [Verfasser:in]; Gage, Victor R. [Verfasser:in]; Sparrow, Stanwood W. [Verfasser:in]
Comparison of Hecter fuel with export aviation gasoline by H. C. Dickinson, V. R. Gage, and S. W. Sparrow
Washington, DC: Gov. Print. Off., 1920

Miller, Roy G. J. [Verfasser:in]
Torsion of wing trusses at diving speeds by Roy G. Miller
Washington, DC: Gov. Print. Off., 1920

Norton, F. H. [Verfasser:in]
The efficiency of small bearings in instruments of the type used in aircraft by F. H. Norton
Washington, DC: Gov. Print. Off., 1920

Parsons, Samuel Reynolds [Verfasser:in]
Properties of special types of radiators by S. R. Parsons
Washington, DC: Gov. Print. Off., [ca. 1920]

Gage, Victor R. [Verfasser:in]; Sparrow, Stanwood W. [Verfasser:in]; Harper, Daniel Roberts [Verfasser:in]
Comparison of alcogas aviation fuel with export aviation gasoline by V. R. Gage, S. W. Sparrow, and D. R. Harper
Washington, DC: Gov. Print. Off., 1920

Nomenclature for aeronautics
Washington, DC: Gov. Print. Off., 1920

Parsons, Samuel Reynolds [Verfasser:in]
Pressure drop in radiator air tubes by S. R. Parsons
Washington, DC: Gov. Print. Off., 1920

Warner, Edward P. [Verfasser:in]; Miller, R. G. [Verfasser:in]
Analysis of wing truss stresses incl. the effect of redundancies by E. P. Warner and R. G. Miller
Washington, DC: Gov. Print. Off., 1920

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