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  1. 1
    Theoretical lift and damping in roll of thin sweptback wings of arbitrary taper and sweep at supersonic speeds : Subsonic leading edges and trailing edges /

    Theoretical lift and damping in roll of thin sweptback wings of arbitrary taper and sweep at supersonic speeds : Subsonic leading edges and trailing edges / by Malvestuto, Frank S.

    Published 1949
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  2. 2
    Some effects of varying the damping in pitch and roll on the flying qualities of a small single-rotor helicopter /

    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
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  3. 3
    Effect of taper ratio on the low-speed rolling stability derivatives of swept and unswept wings of aspect ratio 2.61 /

    Effect of taper ratio on the low-speed rolling stability derivatives of swept and unswept wings of aspect ratio 2.61 / by Brewer, Jack D.

    Published 1951
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  4. 4
    Experimental investigation of rolling performance of straight and sweptback flexible wings with various ailerons /

    Experimental investigation of rolling performance of straight and sweptback flexible wings with various ailerons / by Cole, Henry A.

    Published 1951
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  5. 5
    Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tips. : Subsonic leading edges /

    Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tips. : Subsonic leading edges / by Margolis, Kenneth

    Published 1950
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  6. 6
    A plan-form parameter for correlating certain aerodynamic characteristics of swept wings /

    A plan-form parameter for correlating certain aerodynamic characteristics of swept wings / by Diederich, Franklin W.

    Published 1951
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  7. 7
    Analysis of the effects of wing interference on the tail contributions to the rolling derivatives /

    Analysis of the effects of wing interference on the tail contributions to the rolling derivatives / by Michael, William H.

    Published 1951
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  8. 8
    Theoretical force and moments due to sideslip of a number of vertical tail configurations at supersonic speeds /

    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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  9. 9
    The response of an aeroplane to the application of ailerons and rudders.

    The response of an aeroplane to the application of ailerons and rudders. by Gandy, R. W.

    Published 1943
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  10. 10
    Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds. : Supersonic leading and trailing edges /

    Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds. : Supersonic leading and trailing edges / by Harmon, Sidney M.

    Published 1950
    Government Document Book
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  11. 11
    A method for predicting the stability in roll of automatically controlled aircraft based on the experimental determination of the characteristics of an automatic pilot /

    A method for predicting the stability in roll of automatically controlled aircraft based on the experimental determination of the characteristics of an automatic pilot / by Jones, Robert T. (Robert Thomas), 1910-1999

    Published 1949
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  12. 12
    Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance /

    Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance / by Bamber, M. J

    Published 1934
    Online Access
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  13. 13
    Damping in roll of cruciform and some related delta wings at supersonic speeds /

    Damping in roll of cruciform and some related delta wings at supersonic speeds / by Ribner, H. S. (Herbert S.), 1913-

    Published 1951
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  14. 14
    Theoretical damping in roll and rolling effectiveness of slender cruciform wings /

    Theoretical damping in roll and rolling effectiveness of slender cruciform wings / by Adams, Gaynor J.

    Published 1951
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  15. 15
    On the effect of subsonic trailing edges on damping in roll and pitch of thin sweptback wings in a supersonic stream /

    On the effect of subsonic trailing edges on damping in roll and pitch of thin sweptback wings in a supersonic stream / by Ribner, H. S. (Herbert S.), 1913-

    Published 1950
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  16. 16
    Theoretical lift and damping in roll of thin sweptback tapered wings with raked-in and cross-stream wing tips at supersonic speeds /

    Theoretical lift and damping in roll of thin sweptback tapered wings with raked-in and cross-stream wing tips at supersonic speeds / by Margolis, Kenneth

    Published 1950
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  17. 17
    Effect of an unswept wing on the contribution of unswept-tail configurations to the low-speed static- and rolling-stability derivatives of a midwing airplane model /

    Effect of an unswept wing on the contribution of unswept-tail configurations to the low-speed static- and rolling-stability derivatives of a midwing airplane model / by Letko, William

    Published 1950
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  18. 18
    Estimation of the damping in roll of supersonic-leading-edge wing-body combinations /

    Estimation of the damping in roll of supersonic-leading-edge wing-body combinations / by Tucker, Warren A.

    Published 1950
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  19. 19
    Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tips.

    Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tips. by Harmon, Sidney M.

    Published 1950
    Government Document Book
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  20. 20
    Theory of helicopter damping in ptich or roll and a comparison with flight measurements /

    Theory of helicopter damping in ptich or roll and a comparison with flight measurements / by Amer, Kenneth B.

    Published 1950
    Government Document Book
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