Pt 1: Propulsive characteristics of 2-and 3-bladed adjustable pitch propellers extended to fairly large blade angles; tip loss; blade deflection; wind tunnel wall interference. Pt 2: Airplane characteristics as affected by operation of propulsive system; experimental results and analysis of effect of power on lift, drag, performance, pitching moment, longitudinal stability, and elevator effectiveness.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Wind tunnel tests on high wing monoplane with running propeller


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Russell, J.S. (Autor:in) / McCoy, H.M. (Autor:in) / Millikan, C.B. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1936


    Format / Umfang :

    13 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Wind-tunnel tests on low wing monoplane with propellers running

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


    Wind-tunnel tests on low wing monoplane with propellers running

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



    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