Propulsive thrust and power characteristics were obtained in addition to thrust and torque distributions and flutter characteristics at both positive and negative thrust conditions and with thrust axis inclined; correlation of flutter stresses and aerodynamic section thrust characteristics.


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    Titel :

    Wind-tunnel investigation of stall-flutter characteristics of supersonic-type propeller at positive and negative thrust


    Weitere Titelangaben:

    NASA -- Memo


    Beteiligte:
    Rogallo, V.L. (Autor:in) / Yaggy, P.F. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    66 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Stall Flutter of Sting-Supported Wind Tunnel Models

    Fuykschot, P. H. / Kooi, J. W. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2004


    Stall Flutter of Sting-Supported Wind Tunnel Models

    Fuykschot, Pieter / Kooi, Joost | AIAA | 2004



    Flutter and Stall Flutter of a Rectangular Wing in a Wind Tunnel

    Razak, Norizham Abdul / Andrianne, Thomas / Dimitriadis, Grigorios | AIAA | 2011


    A Model for the Fast Prediction of Propeller Stall Flutter

    Delamore-Sutcliffe, D. / Greenwell, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006