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    National Advisory Committee for Aeronautics | TIBKAT

    National Advisory Committee for Aeronautics, NACA - University Conference on Aerodynamics

    Engineering Index Backfile | 1948
    , and orienting reference material for further study; supersonics, stability and control, and wing characteristics considered. Eng Soc Lib, NY. ...
    Publisher: Durand Reprinting Committee, California Institute of Technology

    Aerodynamic characteristics of airfoils / by National Advisory Committee for Aeronautics ; 3

    TIBKAT | 1923

    The variable density wind tunnel of the national advisory committee for aeronautics

    Munk, M.M. / Miller, E.W. | Engineering Index Backfile | 1926
    Publisher: National Advisory Committee for Aeronautics

    Aerodynamic characteristics of airfoils / by National Advisory Committee for Aeronautics ; 4: Continuation of reports Nos. 93, 124, and 182

    TIBKAT | 1926

    The variable density wind tunnel of the National Advisory Committee for Aeronautics : [part 1 und 2]

    Munk, Max M. / Miller, Elton W. | TIBKAT | 1925

    Preliminary wing model tests in the variable density wind tunnel of the National Advisory Committee for Aeronautics

    Munk, Max M. | TIBKAT | 1925

    Nomenclature for aeronautics

    Engineering Index Backfile | 1920
    Nomenclature and list of symbols approved by Executive Committee of National Advisory Committee for Aeronautics. ...
    Publisher: National Advisory Committee for Aeronautics
    Keywords: Aeronautics

    Applications of modern hydrodynamics to aeronautics

    Prandtl, L. | Engineering Index Backfile | 1921
    Publisher: National Advisory Committee for Aeronautics
    Keywords: Aeronautics

    Bibliography of aeronautics 1923, Paul Brockett

    Engineering Index Backfile | 1926
    Publisher: National Advisory Committee for Aeronautics
    Keywords: Aeronautics

    Systematic two-dimensional cascade tests of NACA 65-series compressor blades at low speeds

    National Advisory Committee for Aeronautics | TIBKAT | 1958

    President's air board reports

    Engineering Index Backfile | 1925
    practical reforms; against a department of national defense and a separate department for aviation; ten recommendations for army and for naval ...
    Keywords: Aviation

    Airfoil section characteristics as affected by variations of Reynolds Number

    Jacobs, E.N. / Sherman, A. | Engineering Index Backfile | 1937
    Publisher: National Advisory Committee for Aeronautics

      Airfoil section characteristics as affected by variations of Reynolds Number

      Jacobs, E.N. / Sherman, A. | Engineering Index Backfile | 1937
      Publisher: National Advisory Committee for Aeronautics

      Airfoil section characteristics as affected by variations of Reynolds Number

      Jacobs, E.N. / Sherman, A. | Engineering Index Backfile
      characteristics with changes in Reynolds Number are inferred and methods of allowing for these variations in practice determined. ...
      Publisher: National Advisory Committee for Aeronautics

    Report on ice formation on aircraft -- By French committee for study of ice formation

    Engineering Index Backfile | 1939
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    A comparison of typical national gas turbine establishment and NACA axial-flow compressor blade sections in cascade at low speed

    Felix, A. Richard / Emery, Hames C. | TIBKAT | 1957
    Publisher: National Advisory Committee for Aeronautics , Washington, DC

    Internal-flow systems for aircraft

    Rogallo, F.M. | Engineering Index Backfile | 1941
    Results of investigation to determine efficient arrangements for internal flow system when such system operates by itself or in combination ...
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Charts for helicopter-performance estimation

    Talkin, H.W. | Engineering Index Backfile | 1945
    Charts for helicopter-performance estimation. (Advance Confidential Report L5E04 Aug 1945) ...
    Publisher: National Advisory Committee for Aeronautics

    Concepts for Safe-Fuel Technology

    Wright, B. R. / National Research Council; Committee on Aviation Fuels with Improved Fire Safety | British Library Conference Proceedings | 1997
    Publisher: National Academy Press
    Keywords: aviation fuels

    Theoretical symmetric span loading at subsonic speeds for wings having arbitrary plan form

    DeYoung, J. / Harper, C.W. | Engineering Index Backfile | 1948
    Theoretical symmetric span loading at subsonic speeds for wings having arbitrary plan form. (35¢) (published 1950) ...
    Publisher: National Advisory Committee for Aeronautics

    Experimental investigation of rectangular exhaust-gas ejectors applicable for engine cooling

    Manganiello, E.J. / Bogatsky, D. | Engineering Index Backfile | 1945
    determined for range of length, aspect ratio, diffusing exit, and shape of exhaust nozzle; ejectors of rectangular cross section were tested because ...
    Publisher: National Advisory Committee for Aeronautics

    Full-scale wind-tunnel and flight tests of Fairchild 22 airplane equipped with zap flap and zap Ailerons

    Dearborn, C.H. / Soulee´ / H.A. | Engineering Index Backfile
    Publisher: National Advisory Committee for Aeronautics

    Potential Surfactant Additives: The Search for the Oxymoron

    Becher, P. / National Research Council; Committee on Aviation Fuels with Improved Fire Safety | British Library Conference Proceedings | 1997
    Publisher: National Academy Press
    Keywords: aviation fuels

    Method for computing leading-edge loads

    Rhode, R.V. / Pearson, H.A. | Engineering Index Backfile | 1931
    Development of formula for determination of proper design load for portion of wing forward of front spar; comparison of results from ...
    Publisher: National Advisory Committee for Aeronautics

    On similarity rules for transonic flows

    Kaplan, C. | Engineering Index Backfile | 1949
    Method used by H.S.TSIEN to derive similarity rules for hypersonic flows is utilized to derive T.vonKARMAN'S similarity rules for transonic ...
    Publisher: National Advisory Committee for Aeronautics

    Stability of castering wheels for aircraft landing gears

    Kantrowitz, A. | Engineering Index Backfile | 1940
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Pressure available for cooling with cowling flaps

    Stickle, G.W. / Naiman, I. / Crigler, J.L. | Engineering Index Backfile | 1941
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Use of source distributions for evaluating theoretical aerodynamics of thin finite wings at supersonic speeds

    Evvard, J.C. | Engineering Index Backfile | 1950
    Use of source distributions for evaluating theoretical aerodynamics of thin finite wings at supersonic speeds. (25¢) ...
    Publisher: National Advisory Committee for Aeronautics

    Experimental investigation of momentum methods for determining profile drag

    Goett, H.J. | Engineering Index Backfile | 1939
    Experimental investigation conducted in ful scale tunnel to determine accuracy of Jones and Betz equations for computing profile drag from ...
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Line vortex theory for calculation of supersonic downwash

    Mirels, H. / Haefeli, R.C. | Engineering Index Backfile | 1949
    Perturbation field induced by line vortex in supersonic stream and downwash behind supersonic lifting surfaces are examined for purpose of ...
    Publisher: National Advisory Committee for Aeronautics

      Line-vortex theory for calculation of supersonic downwash

      Mirels, H. / Haefeli, R.C. | Engineering Index Backfile | 1950
      approximate methods for determining downwash behind supersonic wings. ...
      Publisher: National Advisory Committee for Aeronautics

    Linearized compressible-flow theory for sonic flight speeds

    Heaslet, M.A. / Lomax, H. / Spreiter, J.R. | Engineering Index Backfile | 1950
    Partial differential equation for perturbation velocity potential is examined for free stream Mach numbers close to and equal to one. (20¢) ...
    Publisher: National Advisory Committee for Aeronautics

      Linearized compressible-flow theory for sonic flight speeds

      Heaslet, M.A. / Lomax, H. / Spreiter, J.R. | Engineering Index Backfile | 1949
      Partial differential equation for perturbation velocity potential is examined for free stream Mach numbers close to and equal to one. ...
      Publisher: National Advisory Committee for Aeronautics

    Generalized equations for selection charts for heat exchangers in aircraft

    Tifford, A.N. / Wood, G.P. | Engineering Index Backfile | 1942
    Method of deriving generalized coordinates for selection charts for any type of heat exchanger -- cross flow, counterflow or parallel flow ...
    Publisher: National Advisory Committee for Aeronautics

    Working charts for determination of lift distribution between biplane wings

    Kuhn, P. | Engineering Index Backfile | 1932
    dihedral in upper and lower wings may be properly provided for by utilizing concepts of average stagger and average gap/chord ratio. ...
    Publisher: National Advisory Committee for Aeronautics

    Design of N.A.C.A. Cowlings for radial air-cooled engines

    Stickle, G.W. | Engineering Index Backfile | 1939
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Theory for primary failure of straight centrally loaded columns

    Lundquist, E.E. / Fligg, C.M. | Engineering Index Backfile | 1937
    Publisher: National Advisory Committee for Aeronautics

      Theory for primary failure of straight centrally loaded columns

      Lundquist, E.E. / Fligg, C.M. | Engineering Index Backfile | 1937
      Publisher: National Advisory Committee for Aeronautics

    Theoretical analysis of various thrust-augmentation cycles for turbojet engines

    Lundin, B.T. | Engineering Index Backfile | 1950
    Publisher: National Advisory Committee for Aeronautics

    Critical stresses for plates

    Lundquist, E.E. / Schuette, E.H. | Engineering Index Backfile | 1943
    Critical Stresses for Plates. (Advance Restricted Report 3J27) ...

    Performance charts for turbojet system

    Pinkel, B. / Karp, I.M. | Engineering Index Backfile | 1946
    Performance charts for turbojet system. (Advance Restricted Report E6E14 June 1946) ...
    Publisher: National Advisory Committee for Aeronautics

    Method for calculating heat transfer in laminar flow region of bodies

    Allen, H.J. / Look, B.C. | Engineering Index Backfile | 1947
    on aircraft; comparison of calculated average heat transfer coefficient for nose section of wing of Lockheed 12-A airplane with that ...
    Publisher: National Advisory Committee for Aeronautics

    Recommendations for numerical solution of reinforced-panel and fuselage-ring problems

    Hoff, N.J. / Libby, P.A. | Engineering Index Backfile | 1948
    Publisher: National Advisory Committee for Aeronautics

      Recommendations for numerical solution of reinforced-panel and fuselage-ring problems

      Hoff, N.J. / Libby, P.A. | Engineering Index Backfile | 1949
      Procedures recommended for solving equations of equilibrium of reinforced panels and isolated fuselage rings as represented by external ...
      Publisher: National Advisory Committee for Aeronautics

    General formulas and charts for calculation of airplane performance

    Oswald, W.B. | Engineering Index Backfile | 1932
    Development of formulas for determination of major airplane performance characteristics making no assumption regarding altitude of airplane ...
    Publisher: National Advisory Committee for Aeronautics

    Apparatus for varying effective dihedral in flight with application to study of tolerable dihedral on conventional fighter airplane

    Kauffman, W.M. / Liddell, Jr., C.J. / Smith, A. et al. | Engineering Index Backfile | 1950
    Publisher: National Advisory Committee for Aeronautics

    Charts for determining propeller efficiency

    Crigler, J.L. / Talkin, H.W. | Engineering Index Backfile | 1944
    Charts for determining propeller efficiency. (Advance Confidential Report L4129 Sept 1944) ...
    Publisher: National Advisory Committee for Aeronautics

    Investigation of thermal ice-prevention system for twin-engine transport airplane

    Jones, A.R. | Engineering Index Backfile | 1948
    Investigation of Thermal Ice-Prevention System for Twin-Engine Transport Airplane. (25¢) ...
    Publisher: National Advisory Committee for Aeronautics

    Influence of loading condition on piloting technique for spin recovery for pursuit airplanes

    Soule, H.A. / Seidman, O. | Engineering Index Backfile | 1942
    Influence of Loading Condition on Piloting Technique for Spin Recovery for Pursuit Airplanes. (Restricted Bul) ...
    Publisher: National Advisory Committee for Aeronautics

    Drag and propulsive characteristics of air-cooled engine-nacelle installations for large airplanes

    Silverstein, A. / Wilson, Jr., H.A. | Engineering Index Backfile | 1942
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Theoretical comparison of several methods of thrust augmentation for turbojet engines

    Hall, E.W. / Wilcox, E.C. | Engineering Index Backfile | 1950
    Theoretical comparison of several methods of thrust augmentation for turbojet engines. ...
    Publisher: National Advisory Committee for Aeronautics

    Belt method for measuring pressure distribution

    Corson, Jr., B.W. | Engineering Index Backfile | 1943
    Publisher: National Advisory Committee for Aeronautics

    Theoretical and experimental data for number of NACA 6A-series airfoil sections

    Loftin, Jr., L.K. | Engineering Index Backfile | 1947
    6A-series airfoil sections designed to eliminate trailing edge cusp characteristic of NACA 6-series sections; data presented for NACA 6A ...
    Publisher: National Advisory Committee for Aeronautics

      Theoretical and experimental data for number of NACA 6A-series airfoil sections

      Loftin, Jr., L.K. | Engineering Index Backfile | 1948
      6A series sections designed to eliminate trailing edge cusp which is characteristic of 6 series sections; theoretical data presented for 6A ...
      Publisher: National Advisory Committee for Aeronautics

    Method for studying hunting oscillations of airplane with simple type of automatic control

    Jones, R.T. | Engineering Index Backfile | 1944
    Publisher: National Advisory Committee for Aeronautics

    Flight investigation of lateral control devices for use with full-span flaps

    Soule, H.A. / Mcavoy, W.H. | Engineering Index Backfile | 1935
    Flight tests of 5 lateral control devices for wings with full-span flaps; controllable auxiliary airfoils, external ailerons, upper-surface ...
    Publisher: National Advisory Committee for Aeronautics

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