Search Results - Seidman, Oscar

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  1. 1
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    Comparison of free-spinning wind-tunnel results with corresponding full-scale spin results / by Seidman, Oscar

    Published 1938
    Government Document Book

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  2. 2
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    Free-spinning-tunnel tests of a 1/23.75-scale model of the Douglas DC-3 airplane / by Seidman, Oscar

    Published 1942
    Government Document Book

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  3. 3
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    Elevator stick forces in spins as computed from wind-tunnel measurements / by Seidman, Oscar

    Published 1942
    Government Document Book

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  4. 4
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    Multiengine airplane spin characteristics as indicated by model tests in the free-spinning wind tunnel / by Seidman, Oscar

    Published 1942
    Government Document Book

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  5. 5
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    Spin tests of a low-wing monoplane in flight and in the free-spinning wind tunnel / by Seidman, Oscar

    Published 1940
    Government Document Book

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  6. 6
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    Spinning of large airplanes / by Seidman, Oscar

    Published 1944
    Government Document Book

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  7. 7
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    An Approximate spin design criterion for monoplanes / by Seidman, Oscar

    Published 1939
    Government Document Book

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  8. 8
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    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
    Government Document Book

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  9. 9
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    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
    Government Document Book

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  10. 10
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    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
    Government Document Book

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  11. 11
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    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
    Online Access
    Government Document eBook

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  12. 12
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    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
    Online Access
    Government Document eBook

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  13. 13
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    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
    Online Access
    Government Document eBook

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  14. 14
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    An approximate spin design criterion for monoplanes / by Seidman, Oscar, Donlan, Charles J.

    Published 1939
    Online Access
    Government Document eBook

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  15. 15
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    Spin tests of a low-wing monoplane in flight and in the free-spinning wind tunnel / by Seidman, Oscar, McAvoy, William H.

    Published 1940
    Online Access
    Government Document eBook

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  16. 16
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    Influence of loading condition on piloting technique for spin recovery for pursuit airplanes / by Soule, Hartley A. (Hartley Akin), 1904-1988

    Published 1942
    Other Authors: “…Seidman, Oscar…”
    Government Document Book

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  17. 17
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    Twenty-sixth annual report of the National Advisory Committee for Aeronautics. 1940.

    Published 1942
    Other Authors: “…Seidman, Oscar…”
    Online Access
    Government Document Electronic eBook

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  18. 18
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    Twenty-first annual report of the National Advisory Committee for Aeronautics 1935. Including technical reports nos. 508 to 541.

    Published 1936
    Other Authors: “…Seidman, Oscar…”
    Online Access
    Government Document Electronic eBook

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  19. 19
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    Twenty-fifth annual report of the National Advisory Committee for Aeronautics, 1939. Including technical reports Nos. 645 to 680.

    Published 1940
    Other Authors: “…Seidman, Oscar…”
    Online Access
    Government Document Electronic eBook

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