A hypersonic cruise transport conceptual design is described. The integration of the subsonic, supersonic, and hypersonic propulsion systems with the aerodynamic design of the airframe is emphasized. An evaluation of various configurations of aircraft and propulsion integration concepts, and selection and refinement of a final design are given. This configuration was used as a baseline to compare two propulsion concepts - one using a fixed geometry dual combustion mode scramjet and the other a variable geometry ramjet engine. Both concepts used turbojet engines for takeoff, landing and acceleration to supersonic speed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Hypersonic Cruise Aircraft Propulsion Integration Study, Volume 1


    Beteiligte:
    R. E. Morris (Autor:in) / G. D. Brewer (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    96 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







    AIRFRAME-PROPULSION INTEGRATION METHODOLOGY FOR WAVERIDER-DERIVED HYPERSONIC CRUISE AIRCRAFT DESIGN CONCEPTS

    Javaid, K. H. / Varnavas / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2004