1–20 of 27 hits
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    Working charts for the selection of aluminum alloy propellers of a standard form to operate with various aircraft engines and bodies

    Weick, F.E. | Engineering Index Backfile | 1931
    Charts prepared from full-scale test data obtained in 20-ft. propeller research tunnel; example for use is also given. ...
    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

    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

    Wind-tunnel tests of Clark Y wing with narrow auxiliary airfoil in different positions

    Weick, F.E. / Bamber, M.J. | Engineering Index Backfile | 1932
    /CDmin of 21% of respective values for main Clark Y wing alone. ...
    Publisher: National Advisory Committee for Aeronautics

    Wind-tunnel research comparing lateral control devices, particularly at high angles of attack

    Weick, F.E. / Harris, T.A. / Shortal, J.A. et al. | Engineering Index Backfile | 1932
    IV -- Floating Tip Ailerons on Rectangular Wings; general performance definitely poorer for all of rectangular wings with floating tip ...
    Publisher: National Advisory Committee for Aeronautics

    Wind tunnel research comparing lateral control devices, particularly at high angles of attack -- XII

    Weick, F.E. / Wenzinger, C.J. | Engineering Index Backfile | 1934
    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

    Wind-tunnel tests on combinations of wing with fixed auxiliary airfoils having various chords and profiles

    Weick, F.E. / Sanders, R. | Engineering Index Backfile | 1933
    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

    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

    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

    Wind-tunnel tests of wing flaps suitable for direct control of glide-path angle

    Weick, F.E. | Engineering Index Backfile | 1936
    Preliminary wind tunnel tests of flap arrangements suitable for direct and immediate control of steepness of glide path of airplane; use ...
    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

    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

    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

    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

    Tests of four racing type airfoils in the twenty-foot propeller research tunnel

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

    Wind-tunnel tests of hall high-lift wing

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

    Wind-tunnel tests of fowler variable-area wing

    Weick, F.E. / Platt, R.C. | Engineering Index Backfile | 1932
    ; highest lift coefficient obtained was 3.17 as compared with 1.27 for main wing alone. ...
    Publisher: National Advisory Committee for Aeronautics

    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