Search Results - Bamber, M. J.

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  1. 1
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    Wind tunnel tests on an airfoil equipped with a split flap and a slot / by Bamber, M. J.

    Published 1929
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  2. 2
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    Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance / by Bamber, M. J

    Published 1934
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  3. 3
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    Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model / by Bamber, M. J

    Published 1934
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  4. 4
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    Wind-tunnel tests of several forms of fixed wing slot in combination with a slotted flap on an N.A.C.A. 23012 airfoil / by Bamber, M. J.

    Published 1939
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  5. 5
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    Spinning characteristics of wings. 25 percent stagger ; 0 degree decalage ; gap/chord 1.0 / by Bamber, M. J.

    Published 1935
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  6. 6
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    Effect of changes in aspect ratio, side area, flight-path angle, and normal acceleration on lateral stability / by Bamber, M. J.

    Published 1942
    Government Document Book

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  7. 7
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    Effect of some present-day airplane design trends on requirements for lateral stability / by Bamber, M. J.

    Published 1941
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  8. 8
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    Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model / by Bamber, M. J.

    Published 1934
    Government Document Book

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  9. 9
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    The aerodynamic forces and moments on a spinning model of the F4B-2 airplane as measured by the spinnning balance / by Bamber, M. J.

    Published 1935
    Government Document Book

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  10. 10
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    Spinning characteristics of wings. by Bamber, M. J.

    Published 1935
    Government Document Book

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  11. 11
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    WInd tunnel tests on an airfoil equipped with a split flap and a slot / by Bamber, M. J.

    Published 1929
    Government Document Book

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  12. 12
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    Wind-tunnel investigation of effect of yaw on lateral-stability characteristics. : 1 - Four N.A.C.A. 23012 wings of various plan forms with and without dihedral / by Bamber, M. J.

    Published 1939
    Government Document Book

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  13. 13
    Cover Image

    Wind-tunnel tests of several forms of fixed wing slot in combination with a slotted flap on an N.A.C.A. 23012 airfoil / by Bamber, M. J.

    Published 1939
    Government Document Book

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  14. 14
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    Wind-tunnel investigation of effect of yaw on lateral-stability characteristics. : 2 - Rectangular N.A.C.A. 23012 wing with a circular fuselage and a fin / by Bamber, M. J.

    Published 1939
    Government Document Book

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  15. 15
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    Effect of some present-day airplane design trends on requirements for lateral stability / by Bamber, M. J.

    Published 1941
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    Government Document Book

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  16. 16
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    Spinning characteristics of wings. : V - N.A.C.A. 0009, 23018, and 6718 monoplane wings / by Bamber, M. J.

    Published 1938
    Government Document Book

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  17. 17
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    Spinning characteristics of wings. : IV - Changes in stagger of rectangular Clark Y biplane cellules / by Bamber, M. J.

    Published 1937
    Government Document Book

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  18. 18
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    Spinning characteristics of wings. : III - A rectangular and a tapered Clark Y monoplane wing with rounded tips / by Bamber, M. J.

    Published 1937
    Government Document Book

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  19. 19
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    Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance / by Bamber, M. J.

    Published 1934
    Government Document Book

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  20. 20
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    Effect of stabilizer location upon pitching and yawing moments in spins as shown by tests with the spinning balance / by Bamber, M. J.

    Published 1933
    Government Document Book

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