Conceptual vehicle configuration and propulsion approach for a Mach 6 transport aircraft capable of carring 200 passengers 9260 km was investigated. Wind tunnel test data for various hypersonic transport configurations were examined. Canidates for baseline reference vehicles were selected. An explanation of technical methods which were used and configuration details which were significant in the final vehicle concept are given.


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    Title :

    Hypersonic Cruise Aircraft Propulsion Integration Study, Volume 2


    Contributors:
    R. E. Morris (author) / G. D. Brewer (author)

    Publication date :

    1979


    Size :

    244 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







    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