NASA Technical Note


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Analysis of Three-dimensional Inviscid Supersonic Flow Between a Body and an Outer Wall


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The three-dimensional inviscid supersonic flow equations are solved for the flow over a body located within a duct. Numerical solutions are obtained by use of the reference plane method of characteristics technique. Results of the analysis are compared with experimental test body pressure distributions obtained with an off-design jet stretcher system. The analysis is sufficiently general so that a variety of internal flows may be predicted. A computer program listing and an example problem are presented.




NASA Technical Paper


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NASA Scientific and Technical Reports


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