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)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Large lightweight turbojet engines


    Weitere Titelangaben:

    Soc Automotive Engrs -- J


    Beteiligte:
    Grinyer, C.A. (Autor:in)


    Erscheinungsdatum :

    1957


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    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


    Starters For Turbojet Engines

    DOWNS, WILLIAM D. | SAE Technical Papers | 1951


    Turbojet Engines - Service Experience

    BAILEY, JOHN W. | SAE Technical Papers | 1950