Basis of comparison is engine factor (ratio of engine thrust to weight of propulsion system and payload); maximum speed, rate of climb, maximum altitude, and range determined for each engine as function of aircraft weight; curves show that rocket ramjet and turbojet are superior for high performance short range aircraft; for long range, engines with low specific fuel consumption, like turbofan, produce best overall aircraft.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Comparing aircraft engines by mission requirement and aircraft performance


    Weitere Titelangaben:

    Aero/Space Eng


    Beteiligte:
    Beans, E.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1959


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch





    Aircraft engines

    Drake, Rollen H. | SLUB | 1948


    Aircraft engines

    Linsley, H.E. | Engineering Index Backfile | 1941


    Aircraft engines

    Engineering Index Backfile | 1940


    Aircraft engines

    NTRS | 1977