Solution presented for relation between blade angle, thrust, and torque coefficients of rotor in hovering flight; method can be used for calculation of static thrust and torque of modern variable pitch propellers.


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    Title :

    Static thrust analysis for helicopter rotors and airplane propellers


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1948


    Size :

    7 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Static thrust of airplane propellers

    Diehl, Walter S | NTRS | 1934


    Static thrust of airplane propellers

    Diehl, W.S. | Engineering Index Backfile | 1932


    Static thrust of airplane propellers

    Diehl, Walter S. | TIBKAT | 1932


    Subsonic compressibility corrections for propellers and helicopter rotors

    Laitone, E.V. / Talbot, L. | Engineering Index Backfile | 1953


    The most efficient thrust distribution for airplane propellers

    Bienen, Th. | Engineering Index Backfile | 1925