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'.
Computations in turbulent flows and off-design performance predictions for airframe-integrated scramjets
1977-10-01
Report
No indication
English
Development Of Airframe-Integrated Scramjets
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