Development of current propeller theory and practice to cover range of aircraft speeds between 450 and 550 mph, which, at 36,000 ft represents flight Mach number range of 0.68 to 0.83; comparative efficiencies of propeller turbine and turbojet systems; propeller noise; propeller solidity; blade section characteristics; flutter; blade root sections and spinners; structural strength; future trends.


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    Title :

    Propellers for high-speed aircraft


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1954


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    PROPELLERS FOR HIGH SPEED AIRCRAFT

    JACOBSON, DANIEL H. / ROGERS, ROBERT A. | SAE Technical Papers | 1956


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    Jacobson, D.H. / Rogers, R.A. | Engineering Index Backfile | 1957


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    Aircraft Propellers

    HAVILL, CLINTON H. | SAE Technical Papers | 1929


    Aircraft propellers

    Havill, C.H. | Engineering Index Backfile | 1929