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    An examination of injector/combustor design effects on scramjet performance (1974)
    In:  Other Sources
    Details
    Publication Date: 2019-07-13
    Description: Description of a simplified one-dimensional treatment of fuel injection for supersonic combustor performance analysis. Representative mixing efficiency variations for both parallel and cross-stream injection are obtained, and approximate means for estimating the length required for complete mixing are demonstrated. Comparisons of calculated and measured data show good agreement.
    Keywords: PROPULSION SYSTEMS
    Type: International Symposium on Air Breathing Engines; Mar 24, 1974 - Mar 29, 1974; Sheffield
    Format: text
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