Showing 1 - 20 results of 143 for search '', query time: 0.15s Refine Results
  1. 1
    On the estimation of jet-induced fountain lift and additional suckdown in hover for two-jet configurations
    Published 1991

    Government Document Book
  2. 2
    On the anomalies in single-jet hover suckdown data
    Published 1991

    Government Document Book
  3. 3
    Light airplane crash tests at three pitch angles /
    by Vaughan, Victor L
    Published 1979

    Government Document Book
  4. 4
    An Advanced pitch change mechanism incorporating a hybrid traction drive
    Published 1984

    Government Document Book
  5. 5
    Computer programs for calculation of sting pitch and roll angles required to obtain angles of attack and sideslip on wind tunnel models
    by Peterson, John B
    Published 1988

    Government Document Book
  6. 6
    Predicted pitching moment of an X29A aircraft
    by Budd, Gerald D
    Published 1987

    Government Document Book
  7. 7
    Computer programs for the calculation of dual sting pitch and roll angles required for an articulated sting to obtain angles of attack and sideslip on wind-tunnel models
    by Peterson, John B
    Published 1991

    Government Document Book
  8. 8
    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
  9. 9
    Aerodynamic characteristics at Reynolds numbers of 3,000,000 and 6,000,000 of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section /
    by Smith, Hamilton A
    Published 1950

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  10. 10
    Hovering and low-speed performance and control characteristics of an aerodynamic-servocontrolled helicopter rotor system as determined on the Langley helicopter tower /
    by Carpenter, Paul J
    Published 1950

    Government Document Book
  11. 11
    Low-speed investigation of a thin, faired, double-wedge airfoil section with nose flaps of various chords /
    by Rose, Leonard M
    Published 1950

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  12. 12
    Time-dependent downwash at the tail and the pitching moment due to normal acceleration at supersonic speeds /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  13. 13
    Some effects of varying the damping in pitch and roll on the flying qualities of a small single-rotor helicopter /
    by Reeder, John P
    Published 1952

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  14. 14
    Damping in pitch and roll of triangular wings at supersonic speeds /
    by Brown, Clinton E
    Published 1948

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  15. 15
    Aerodynamic characteristics of a number of modified NACA four-digit-series airfoil sections /
    by Loftin, Laurence K
    Published 1948

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  16. 16
    Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experiment /
    by Runyan, Harry L
    Published 1951

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  17. 17
    The Indicial lift and pitching moment for a sinking or pitching two-dimensional wing flying at subsonic or supersonic speeds /
    by Lomax, Harvard
    Published 1951

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  18. 18
    Three-dimensional unsteady lift problems in high-speed flight : The triangular wing /
    by Lomax, Harvard
    Published 1951

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  19. 19
    An Investigation of the effects of jet-outlet cut-off angle on thrust direction and body pitching moment /
    by Blackaby, James R
    Published 1951

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  20. 20
    A Generalized theoretical investigation of the hydrodynamic pitching moments experienced by V-bottom seaplanes during step-landing impacts and comparisons with experiment /
    by Milwitzky, Benjamin
    Published 1948

    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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