Performance of engines in both subsonic and supersonic flight in relation to aircraft requirements; advantages and disadvantages of bypass engines and small turbojet in relation to large straight jet engine of 18,000-lb thrust: improvement in thrust/weight ratio of large engines made possible by use of titanium, and potentialities of ejector nozzles and turbine blade cooling. (See also Soc Automotive Engrs -- Paper n 81 Apr 2-5 1957 25 p; abstracts in Automotive Industries v 116 n 9 May 1 1957 p 136)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Large lightweight turbojet engines


    Additional title:

    Soc Automotive Engrs -- J


    Contributors:


    Publication date :

    1957


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Large Lightweight Turbojet Engines

    Grinyer, C. A. | SAE Technical Papers | 1958


    Large lightweight turbojet engines

    Grinyer, C.A. | Engineering Index Backfile | 1957


    Large lightweight turbojet engines

    Grinyer, C.A. | Engineering Index Backfile | 1957


    Afterburners for turbojet engines

    Cleveland, F.A. | Engineering Index Backfile | 1948


    Starters For Turbojet Engines

    DOWNS, WILLIAM D. | SAE Technical Papers | 1951