Purpose of tests was to determine (1) effect of power on static longitudinal stability (elevator free), (2) effect of power on elevator hinge moments (at various tab angles), and (3) effect of power on static directional stability with model operating at high and low angle of attack. Before Inst Aeronautical Sciences.


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    Title :

    Wind-tunnel tests on low wing monoplane with propellers running


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Miller, S.S. (author) / Albach, W.H. (author)

    Published in:

    Publication date :

    1938


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Wind-tunnel tests on low wing monoplane with propellers running

    Miller, S.S. / Albach, W.H. | Engineering Index Backfile | 1938


    Wind tunnel tests on high wing monoplane with running propeller

    Russell, J.S. / McCoy, H.M. / Millikan, C.B. | Engineering Index Backfile | 1936


    Wind Tunnel Tests on a Model of a Monoplane Wing with Floating Ailerons

    Knight, Montgomery / Bamber, Millard J | NTRS | 1929


    Wind tunnel tests on a model of a monoplane wing with floating allerons

    Knight, Montgomery ;Bamber, Millard J. | SLUB | 1929


    Wind tunnel tests on a model of a monoplane wing with floating ailerons

    Knight, M. / Bamber, M.J. | Engineering Index Backfile | 1929