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  1. 1
    Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles /
    by Mason, Mary L
    Published 1985

    Government Document Book
  2. 2
    Tests on an airfoil with two slots suitable for an aircraft of high performance : lift, drag, rolling and yawing moment measurements /
    by Page, F. Handley
    Published 1926

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  3. 3
    Determination of the air forces and moments produced by the ailerons of an airplane /
    by Wieselsberger, C
    Published 1928

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  4. 4
    Combined pitching and yawing motion of airplanes /
    by Von Baranoff, A
    Published 1931

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  5. 5
    Effect of fuselage and tail surfaces on low-speed yawing characteristics of a swept-wing model as determined in curved-flow test section of Langley stability tunnel /
    by Bird, John D
    Published 1951

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    Government Document Book
  6. 6
    Experimental investigation of the pressure distribution about a yawed circular cylinder in the critical Reynolds number range /
    by Bursnall, William J
    Published 1951

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    Government Document Book
  7. 7
    Effect of yaw at supersonic speeds on theoretical aerodynamic coefficients of thin pointed wings with several types of trailing edge /
    by Moeckel, W. E
    Published 1948

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    Government Document Book
  8. 8
    Theoretical force and moments due to sideslip of a number of vertical tail configurations at supersonic speeds /
    by Martin, John C
    Published 1951

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    Government Document Book
  9. 9
    Bench-test investigation of the transient-response characteristics of several simulated airplanes incorporating an autopilot sensitive to yawing accelerations /
    by Howard, Donald A
    Published 1951

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    Government Document Book
  10. 10
    Forces and moments on a yawed airfoil /
    by Hoener, Sighard
    Published 1939

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    Government Document Book
  11. 11
    Measurements on a low-wing model in the rotating jet and comparison with flight measurements /
    by Bader, W
    Published 1939

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    Government Document Book
  12. 12
    Pressure distribution measurements at high speed and oblique incidence of flow /
    by Lippisch, Alexander, 1894-1976
    Published 1947

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    Government Document Book
  13. 13
    Investigations of lateral stability of a glide bomb using automatic control having no time lag /
    by Sponder, E. W
    Published 1950

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    Government Document Book
  14. 14
    Calculation of potential flow past airship bodies in yaw /
    by Lotz, I
    Published 1932

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    Government Document Book
  15. 15
    Total-head meter with small sensitivity to yaw /
    by Kiel, G
    Published 1935

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    Government Document Book
  16. 16
    Some effects of aspect ratio and tail length on the contribution of a vertical tail to unsteady lateral damping and directional stability of a model oscillating continuously in yaw /
    by Fisher, Lewis R
    Published 1954

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  17. 17
    Theoretical supersonic force and moment coefficients on a sideslipping vertical- and horizontal-tail combination with subsonic leading edges and supersonic trailing edges /
    by Malvestuto, Frank S
    Published 1954

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    Government Document Book
  18. 18
    A simple mechanical analogue for studying the dynamic stability of aircraft having nonlinear moment characteristics /
    by Canning, Thomas N
    Published 1954

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    Government Document Book
  19. 19
    Some effects of frequency on the contribution of a vertical tail to the free aerodynamic damping of a model oscillating in yaw /
    by Bird, John D
    Published 1952

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    Government Document Book
  20. 20
    Theoretical calculations of the pressures, forces, and moments due to various lateral motions acting on thin isolated vertical tails with supersonic leading and trailing edges /
    by Margolis, Kenneth
    Published 1955

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
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