Showing 1 - 15 results of 15 for search 'Bird, J. D.', query time: 0.08s Refine Results
  1. 1
    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 /

    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, J. D.

    Published 1951
    Government Document Book
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  2. 2
    Some experiments on visualization of flow fields behind low-aspect-ratio wings by means of a tuft grid /

    Some experiments on visualization of flow fields behind low-aspect-ratio wings by means of a tuft grid / by Bird, J. D.

    Published 1952
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  3. 3
    Some calculations of the lateral response of two airplanes to atmospheric turbulence with relation to the lateral snaking problem /

    Some calculations of the lateral response of two airplanes to atmospheric turbulence with relation to the lateral snaking problem / by Bird, J. D.

    Published 1955
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  4. 4
    Some effects of frequency on the contribution of a vertical tail to the free aerodynamic damping of a model oscillating in yaw /

    Some effects of frequency on the contribution of a vertical tail to the free aerodynamic damping of a model oscillating in yaw / by Bird, J. D.

    Published 1952
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  5. 5
    Investigation of the influence of fuselage and tail surfaces on low-speed static stability and rolling characteristics of a swept-wing model /

    Investigation of the influence of fuselage and tail surfaces on low-speed static stability and rolling characteristics of a swept-wing model / by Bird, J. D.

    Published 1952
    Government Document Book
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  6. 6
    Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil /

    Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil / by Bird, J. D.

    Published 1945
    Government Document Book
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  7. 7
    Wind-tunnel tests of a blunt-nose aileron with beveled trailing edge on an NACA 66(215)-216 airfoil with several modifications of aileron nose and adjacent airfoil contour /

    Wind-tunnel tests of a blunt-nose aileron with beveled trailing edge on an NACA 66(215)-216 airfoil with several modifications of aileron nose and adjacent airfoil contour / by Bird, J. D.

    Published 1945
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  8. 8
    Wind-tunnel tests of a piston-type control booster on an airfoil and aileron model /

    Wind-tunnel tests of a piston-type control booster on an airfoil and aileron model / by Bird, J. D.

    Published 1943
    Government Document Book
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  9. 9
    Frequency of encounter of aircraft in a random horizontal field /

    Frequency of encounter of aircraft in a random horizontal field / by Bird, J. D.

    Published 1976
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  10. 10
    Some theoretical low-speed span loading characteristics of swept wings in roll and sideslip /

    Some theoretical low-speed span loading characteristics of swept wings in roll and sideslip / by Bird, J. D.

    Published 1949
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  11. 11
    A study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results /

    A study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results / by Bird, J. D.

    Published 1950
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  12. 12
    Wind-tunnel tests of hinge-moment characteristics of spring-tab ailerons /

    Wind-tunnel tests of hinge-moment characteristics of spring-tab ailerons / by Imlay, Frederick H.

    Published 1944
    Other Authors: “…Bird, J. D.…”
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  13. 13
    WInd-tunnel tests of ailerons at various speeds. : 2 - Ailerons of 0.20 airfoil chord and true contour with 0.60 aileron-chord sealed internal balance on the NACA 66,2-216 airfoil /

    WInd-tunnel tests of ailerons at various speeds. : 2 - Ailerons of 0.20 airfoil chord and true contour with 0.60 aileron-chord sealed internal balance on the NACA 66,2-216 airfoil... by Denaci, H. G.

    Published 1943
    Other Authors: “…Bird, J. D.…”
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  14. 14
    Thirty-sixth annual report of the National Advisory Committee for Aeronautics, 1950. Including technical reports Nos. 951 to 1002.

    Thirty-sixth annual report of the National Advisory Committee for Aeronautics, 1950. Including technical reports Nos. 951 to 1002.

    Published 1951
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  15. 15
    Thirty-seventh annual report of the National Advisory Committee for Aeronautics. 1951. Including technical reports nos. 1003 to 1058

    Thirty-seventh annual report of the National Advisory Committee for Aeronautics. 1951. Including technical reports nos. 1003 to 1058

    Published 1952
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