General problems associated with design of propellers for gas turbines and application of turbine propeller power plants to high speed airplanes; conclusion reached that at speeds of 600 to 700 mph propeller efficiencies of over 70% appear possible, particularly with unconventional configurations, such as swept-back blades and small diameter multi-blade propellers. Before Inst Aeronautical Sciences.


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    Title :

    Propellers for aircraft gas turbines


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Brady, G.W. (author)


    Publication date :

    1946


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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