In 1998, in the wake of the successful Working Group (WG) 18, the new RTO AVT Panel endorsed the creation of a new WG on 'Technologies for Propelled Hypersonic Flight', RTO AVT WG 10. Three (3) Subgroups were created to structure the activities of the Working Group. Subgroup 2 addressed the physical modelling aspects associated with scram combustion; a review was given on fuels, turbulence mixing, ignition and flame holding prediction capabilities as well as vitiation. This report documents the results of the Applied Vehicle Technology Panel Working Group 10, Subgroup 2.


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    Title :

    Technologies for Propelled Hypersonic Flight Volume 2 - Subgroup 2: Scram Propulsion


    Contributors:
    J. Muylaert (author) / A. Kumar (author) / P. Drummond (author) / M. Bouchez (author) / C. R. McClinton (author)

    Publication date :

    2006


    Size :

    211 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Technologies for propelled hypersonic flight : [plug nozzles - scram propulsion - CFD validation for hypersonic flight]

    Research and Technology Organization, Applied Vehicle Technology Panel | TIBKAT | 2006



    Inlet and Propulsion Integration of SCRAM Propelled Vehicles

    Povinelli, L. A. / North Atlantic Treaty Organization; Advisory Group for Aerospace Research &Development; Fluid Dynamics Panal | British Library Conference Proceedings | 1996


    Configurational Aerothermodynamics of RAM and SCRAM Propelled Vehicles

    Perrier, P. / Courty, J. C. / North Atlantic Treaty Organization; Advisory Group for Aerospace Research &Development; Fluid Dynamics Panal | British Library Conference Proceedings | 1996


    INTERNATIONAL EFFORTS SCRAM INTO FLIGHT

    Hicks, John W. | Online Contents | 1998