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  1. 1
    Investigation at low speed of 45 degrees and 60 degrees sweptback, tapered, low-drag wings equipped with various types of full-span, trailing-edge flaps /
    by Harper, John J
    Published 1951

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    Government Document Book
  2. 2
    Six-component measurements on a straight and a 35 degree swept-back trapezoidal wing with and without split flap /
    by Thiel, G
    Published 1947

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    Government Document Book
  3. 3
    Force and pressure-distribution measurements on a rectangular wing with a slotted droop nose and with either plain and split flaps in combination or a slotted flap /
    by Lemme, H. G
    Published 1947

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    Government Document Book
  4. 4
    Lift and pitching moment at low speeds of the NACA 64A010 airfoil section equipped with various combinations of a leading-edge slat, leading-edge flap, split flap, and double-slotted flap /
    by Kelly, John A
    Published 1953

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    Government Document Book
  5. 5
    Wind-tunnel investigation of effects of ground proximity and split flaps on the lateral stability derivatives of a 60 degrees delta-wing model oscillating in yaw /
    by Jaquet, Byron M
    Published 1957

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    Government Document Book
  6. 6
    The Effect of partial-span split flaps on the aerodynamic characteristics of a Clark Y wing /
    by Wenzinger, Carl J
    Published 1933

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    Government Document Book
  7. 7
    Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model /
    by Bamber, Millard J
    Published 1934

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    Government Document Book
  8. 8
    A Method of estimating the aerodynamic effects of ordinary and split flaps of airfoils similar to the Clark Y /
    by Pearson, H. A
    Published 1936

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  9. 9
    Pressure distribution over a Clark Y-H airfoil section with a split flap /
    by Wenzinger, Carl J
    Published 1937

    Government Document Book
  10. 10
    Effects of compressibility on normal-force, pressure, and load characterstics of a tapered wing of NACA 66-series airfoil sections with split flaps /
    by West, F. E
    Published 1948

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  11. 11
    A study of several factors affecting the stability contributed by a horizontal tail at various vertical positions on a sweptback-wing airplane model /
    by Foster, Gerald V
    Published 1956

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    Government Document Book
  12. 12
    Pressure-distribution measurements on a tapered wing with a partial-span split flap in curved flight /
    by Troller, T
    Published 1939

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    Government Document Book
  13. 13
    Wind-tunnel investigation of rectangular and tapered N.A.C.A. 23012 wings with plaine ailerons and full-span split flaps /
    by Wenzinger, Carl J
    Published 1938

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    Government Document Book
  14. 14
    Pressure-distribution measurements on a tapered wing with full-span split flap in curved flight /
    by Troller, T
    Published 1939

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  15. 15
    Pressure-distribution measurements on a rectangular wing with a partial-span split flap in curved flight /
    by Rokus, Frank G
    Published 1939

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    Government Document Book
  16. 16
    Interference of wing and fuselage from tests of 18 combinations in the N.A.C.A. variable-density tunnel combinations with split flaps /
    by Sherman, Albert
    Published 1938

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    Government Document Book
  17. 17
    Wind-tunnel tests of a Clark-Y wing having split flaps with gaps /
    by Wenzinger, Carl J
    Published 1938

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    Government Document Book
  18. 18
    The Effect of split trailing-edge wing flaps on the aerodynamic characteristics of a parasol monoplane /
    by Wallace, Rudolf N
    Published 1933

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    Government Document Book
  19. 19
    Wind-tunnel measurements of air loads on split flaps /
    by Wenzinger, Carl J
    Published 1934

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    Government Document Book
  20. 20
    The Aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear /
    by Weick, Fred A
    Published 1932

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
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