Showing 1 - 18 results of 18 for search 'Neihouse, A. I.', query time: 0.06s Refine Results
  1. 1
    Dynamic similitude between a model and a full-scale body for model investigation at full-scale Mach number /

    Dynamic similitude between a model and a full-scale body for model investigation at full-scale Mach number / by Neihouse, A. I.

    Published 1950
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  2. 2
    Spin-tunnel investigation to determine the effectiveness of a rocket for spin recovery /

    Spin-tunnel investigation to determine the effectiveness of a rocket for spin recovery / by Neihouse, A. I.

    Published 1949
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  3. 3
    The aileron as an aid to recovery from the spin /

    The aileron as an aid to recovery from the spin / by Neihouse, A. I.

    Published 1940
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  4. 4
    A mass-distribution criterion for predicting the effect of control manipulation on the recovery from a spin /

    A mass-distribution criterion for predicting the effect of control manipulation on the recovery from a spin / by Neihouse, A. I.

    Published 1942
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  5. 5
    The Aileron as an aid to recovery from the spin /

    The Aileron as an aid to recovery from the spin / by Neihouse, A. I.

    Published 1940
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  6. 6
    Status of spin research for recent airplane designs /

    Status of spin research for recent airplane designs / by Neihouse, A. I.

    Published 1960
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  7. 7
    Effect of wing leading-edge slots on the spin and recovery characteristics of airplanes /

    Effect of wing leading-edge slots on the spin and recovery characteristics of airplanes / by Neihouse, A. I.

    Published 1943
    Government Document Book
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  8. 8
    Tail-design requirements for satisfactory spin recovery /

    Tail-design requirements for satisfactory spin recovery / by Neihouse, A. I.

    Published 1946
    Government Document Book
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  9. 9
    Tail-design requirements for satisfactory spin recovery for personal-owner-type light airplanes /

    Tail-design requirements for satisfactory spin recovery for personal-owner-type light airplanes / by Neihouse, A. I.

    Published 1947
    Government Document Book
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  10. 10
    The Effect of variations in moments of inertia on spin and recovery characteristics of a single-engine low-wing monoplane with various tail arrangements including a twin tail /

    The Effect of variations in moments of inertia on spin and recovery characteristics of a single-engine low-wing monoplane with various tail arrangements including a twin tail / by Neihouse, A. I.

    Published 1948
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  11. 11
    Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails.

    Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. by Seidman, Oscar, Neihouse, A. I.

    Published 1937
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  12. 12
    Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails.

    Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. by Seidman, Oscar, Neihouse, A. I.

    Published 1938
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  13. 13
    Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails.

    Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. by Seidman, Oscar, Neihouse, A. I.

    Published 1937
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  14. 14
    Comparison of free-spinning wind-tunnel results with corresponding full-scale spin results /

    Comparison of free-spinning wind-tunnel results with corresponding full-scale spin results / by Seidman, Oscar

    Published 1938
    Other Authors: “…Neihouse, A. I.…”
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  15. 15
    Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. : 1. Basic loading condition /

    Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. : 1. Basic loading condition / by Seidman, Oscar

    Published 1937
    Other Authors: “…Neihouse, A. I.…”
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  16. 16
    Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. : II. Mass distributed along the fuselage /

    Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. : II. Mass distributed along the fuselage / by Seidman, Oscar

    Published 1937
    Other Authors: “…Neihouse, A. I.…”
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  17. 17
    Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. : III. Mass distributed along the wings /

    Free-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails. : III. Mass distributed along the wings / by Seidman, Oscar

    Published 1938
    Other Authors: “…Neihouse, A. I.…”
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  18. 18
    Twenty-sixth annual report of the National Advisory Committee for Aeronautics. 1940.

    Twenty-sixth annual report of the National Advisory Committee for Aeronautics. 1940.

    Published 1942
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