Relative merits of gas turbines and piston engines in helicopters; advantages of turbine are its good specific weight, little vibration, low frontal area and ability to use fuels other than gasoline; three different engine/rotor systems analyzed -- shaft drive, ducted gas and ducted air schemes. From paper before Helicopter Assn.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Gas turbines for helicopters


    Additional title:

    Aeroplane


    Contributors:
    Brown, J. (author)

    Published in:

    Aeroplane ; 87 , n 2257


    Publication date :

    1954


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Gas turbines for helicopters

    Morley, A.W. / Cushing, W.R. | Engineering Index Backfile | 1960


    Napier turbines for helicopters

    Morley, A.W. | Engineering Index Backfile | 1955


    Gas turbines for helicopters

    Morley, A.W. | Engineering Index Backfile | 1958


    Shaft gas turbines for helicopters

    Miller, Jr., W.S. / Krebs, R.P. / Blaschke, T.C. | Engineering Index Backfile | 1955


    Shaft Gas Turbines For Helicopters

    Krebs, R. P. / Blaschke, T. C. / Miller, W. S. | SAE Technical Papers | 1956