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Wenzinger, C.J.   Weick, F.E.   Physics   Chemical and environmental engineering   Print   Clear all
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    Aerodynamic characteristics of model wing having split flap deflected downward and moved to rear

    Weick, F.E. / Harris, T.A. | Engineering Index Backfile | 1932
    Publisher: National Advisory Committee for Aeronautics

    Aerodynamic characteristics of slotted clark Y wing as affected by auxiliary airfoil position

    Wenzinger, C.J. / Shortal, J.A. | Engineering Index Backfile | 1931
    Aerodynamic force tests conducted in vertical wind tunnel; increase of 41.5 per cent in max. lift; angle of attack for max. lift increased ...
    Publisher: National Advisory Committee for Aeronautics

    Aerodynamic tests of low aspect ratio tapered wing with various flaps, for use on tailless airplanes

    Weick, F.E. / Sanders, R. | Engineering Index Backfile | 1933
    for tailless airplanes. ...
    Publisher: National Advisory Committee for Aeronautics

    Characteristics of Clark Y wing model equipped with several forms of low-drag fixed slots

    Weick, F.E. / Wenzinger, C.J. | Engineering Index Backfile | 1932
    Investigation to develop low-drag fixed slot for airplane wing which would avoid complications and maintenance difficulties of present ...
    Publisher: National Advisory Committee for Aeronautics

    Development of N.A.C.A. Slot-lip aileron

    Weick, F.E. / Shortal, J.A. | Engineering Index Backfile | 1935
    Publisher: National Advisory Committee for Aeronautics

    Drag and cooling with various forms of cowling for a "whirlwind" engine in a cabin fuselage

    Weick, F.E. | Engineering Index Backfile | 1928
    Results of investigation in 20-ft. propeller tunnel on engines entirely exposed up to completely cowled types; careful design for proper ...
    Publisher: National Advisory Committee for Aeronautics

    Drag testing. Full scale drag tests on various parts of sperry messenger airplane

    Weick, F.E. | Engineering Index Backfile | 1928
    Publisher: National Advisory Committee for Aeronautics

    Effect of multiple fixed slots and trailing-edge flap on lift and drag of Clark Y airfoil

    Weick, F.E. / Shortal, J.A. | Engineering Index Backfile | 1932
    Publisher: National Advisory Committee for Aeronautics

    Effect of partial-span split flaps on aerodynamic characteristics of clark Y wing

    Wenzinger, C.J. | Engineering Index Backfile | 1933
    Publisher: National Advisory Committee for Aeronautics

    Effect on lift, drag, and spinning characteristics of sharp leading edges on airplane wings

    Weick, F.E. / Scudder, N.E. | Engineering Index Backfile | 1933
    Publisher: National Advisory Committee for Aeronautics

    Effects of full-span and partial-span split flaps on aerodynamic characteristics of tapered wing

    Wenzinger, C.J. | Engineering Index Backfile | 1934
    Aerodynamic force tests made in wind tunnel using highly tapered Clark Y wing equipped with various split flaps; results given for both ...
    Publisher: National Advisory Committee for Aeronautics

    Flight investigation of lateral control characteristics of short wide ailerons and various spoilers with different amounts of wing dihedral

    Weick, F.E. / Soule, H.A. / Gough, M.N. | Engineering Index Backfile | 1934
    Publisher: National Advisory Committee for Aeronautics

    Full scale investigation of the drag of a wing radiator

    Weick, F.E. | Engineering Index Backfile | 1929
    Publisher: National Advisory Committee for Aeronautics

    Full scale tests of wood propellers on A VE-7 airplane in the propeller research tunnel

    Weick, F.E. | Engineering Index Backfile | 1929
    Publisher: National Advisory Committee for Aeronautics

    Full scale tests on a thin metal propeller at various tip speeds

    Weick, F.E. | Engineering Index Backfile | 1929
    Publisher: National Advisory Committee for Aeronautics

    Full scale wind tunnel tests with a series of propellers of different diameters on a single fuselage

    Weick, F.E. | Engineering Index Backfile | 1930
    -cockpit fuselage; tests were made in 20-ft. propeller research tunnel of National Advisory Committee for Aeronautics; results show little ...
    Publisher: National Advisory Committee for Aeronautics

    Preliminary investigation of modifications to conventional airplanes to give nonstalling and short-landing characteristics

    Weick, F.E. | Engineering Index Backfile | 1932
    Publisher: National Advisory Committee for Aeronautics

    Preliminary wind-tunnel investigation of N.A.C.A. 23012 airfoil with various arrangements of venetian-blind flaps

    Wenzinger, C.J. / Harris, T.A. | Engineering Index Backfile | 1940
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

    Pressure distribution over airfoil section with flap and tab

    Wenzinger, C.J. | Engineering Index Backfile | 1936
    Publisher: National Advisory Committee for Aeronautics

    Pressure distribution over airfoils with fowler flaps

    Wenzinger, C.J. / Anderson, W.B. | Engineering Index Backfile | 1938
    Publisher: National Advisory Committee for Aeronautics (United States Advisory Committee for Aeronautics)

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