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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    Title :

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


    Contributors:
    R. J. Jackson (author) / T. T. Wang (author)

    Publication date :

    1974


    Size :

    30 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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