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; Soc Automotive Engrs -- J v 65 n 10 Sept 1957 p 25-6)


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    Titel :

    Large lightweight turbojet engines


    Weitere Titelangaben:

    Automotive Industries


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

    Erschienen in:

    Erscheinungsdatum :

    1957


    Format / Umfang :

    136 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Large lightweight turbojet engines

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


    Large Lightweight Turbojet Engines

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


    Large lightweight turbojet engines

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


    J79 Turbojet Engines

    E. W. Lindner | NTIS | 1959


    Starters For Turbojet Engines

    DOWNS, WILLIAM D. | SAE Technical Papers | 1951