The research activity focused on two main tasks: (1) the further development of the SCRAM program and, in particular, the addition of a procedure for modeling the mechanism of the internal adjustment process of the flow, in response to the imposed thermal load across the combustor and (2) the development of a numerical code for the computation of the variation of concentrations throughout a turbulent field, where finite-rate reactions occur. The code also includes an estimation of the effect of the phenomenon called 'unmixedness'.


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    Title :

    Computations in turbulent flows and off-design performance predictions for airframe-integrated scramjets


    Contributors:

    Publication date :

    1977-10-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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