This survey of supersonic combustion ramjet (scramjet) engine development in the United States covers development of this unique engine cycle from its inception in the early 1960's through the various programs currently being pursued and, in some instances, describing the future direction of the programs. These include developmental efforts supported by the U.S. Navy, National Aeronautics and Space Administration, and U.S. Air Force. Results of inlet, combustor, and nozzle component tests, free-jet engine tests, analytical techniques developed to analyze and predict component and engine performance, and flight-weight hardware development are presented. These results show that efficient scramjet propulsion is attainable in a variety of flight configurations with a variety of fuels. Since the scramjet is the most efficient engine cycle for hypersonic flight within the atmosphere, it should be given serious consideration in future propulsion schemes


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Supersonic combustion ramjet /scramjet/ engine development in the United States


    Beteiligte:
    Waltrup, P. J. (Autor:in) / Anderson, G. Y. (Autor:in) / Stull, F. D. (Autor:in)

    Kongress:

    International Symposium on Air Breathing Engines ; 1976 ; Munich, Germany


    Erscheinungsdatum :

    01.01.1976


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Ramjet and Scramjet Engine

    Babu, V. | Springer Verlag | 2021


    Critical considerations in the design of supersonic combustion ramjet /scramjet/ engines

    WALTRUP, P. J. / BILLIG, F. S. / EVANS, M. C. | AIAA | 1981


    Experimental Investigation of the Combustion Process in a Supersonic Combustion Ramjet (SCRAMJET)

    Waidmann, W. / Alff, F. / Brummund, U. et al. | British Library Conference Proceedings | 1994