A computer program was developed to describe the performance of ramjet and scramjet cycles. The program performs one dimensional calculations of the equilibrium, real-gas internal flow properties of the engine. The program can be used for the following: (1) preliminary design calculation and (2) design analysis of internal flow properties corresponding to stipulated flow areas. Only the combustion of hydrogen in air is considered in this case. (Author)


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    Titel :

    Hypersonic Ramjet Experiment Project. Phase 1: Computer Program Description, Ramjet and Scramjet Cycle Performance


    Beteiligte:
    R. J. Jackson (Autor:in) / T. T. Wang (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    30 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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