This report describes the experimental data and the procedures used in acquiring and reducing the thermal loads data during tests of a hydrocarbon- fueled scramjet combustor at United Technologies Research Center (UTRC). This research effort is part of the UTRC effort to develop dual-mode scramjet combustor technology to support the development of Mach S missile technology. The objective of the thermal loads testing was to map the thermal and mechanical loads, including heat transfer, dynamic and static pressures, and skin friction in a scramjet combustor during direct-connect scramjet tests. The tests were conducted at the UTRC Ramject/Scramjet direct-connect combustor test facility in East Hartford, CT.


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    Title :

    Thermal Performance of a Scramjet Combustor Operating at Mach 5.6 Flight Conditions


    Contributors:

    Publication date :

    1997


    Size :

    145 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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