A methodology for using optimization in designing metallic cooling jackets for scramjet engines is presented. The optimal design minimizes the required coolant flow rate subject to temperature, mechanical-stress, and thermal-fatigue-life constraints on the cooling-jacket panels, and Mach-number and pressure contraints on the coolant exiting the panel. The analytical basis for the methodology is presented, and results for the optimal design of panels are shown to demonstrate its utility.


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    Titel :

    Active cooling design for scramjet engines using optimization methods


    Beteiligte:

    Erscheinungsdatum :

    01.03.1988


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Active cooling design for scramjet engines using optimization methods

    SCOTTI, STEPHEN / MARTIN, CARL / LUCAS, STEPHEN | AIAA | 1988


    Active Cooling Design for Scramjet Engines Using Optimization Methods

    S. J. Scotti / C. J. Martin / S. H. Lucas | NTIS | 1988



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    Full Flow-Path Optimization of Axisymmetric Scramjet Engines

    Ogawa, H. / Alazet, Y. / Pudsey, A. et al. | British Library Conference Proceedings | 2011