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- W2064203216 abstract "Rocket plume exhaust structures are aerodynamically and thermochemically very complex and the prediction of plume properties such as temperature, velocity, pressure, chemical species concentrations and turbulence properties is a formidable task as there are no definitive models for viscous and chemical effects. Contemporary computational techniques are still in their infancy and cannot yet reliably predict plume properties. Only through validation of computer codes using experimental data, can computational models be developed to the point where they can be confidently used as design and predictive tools. The motivation for this study was to acquire well defined data for rocket plumes at low altitude hypersonic flight conditions so that the above issues could be investigated." @default.
- W2064203216 created "2016-06-24" @default.
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- W2064203216 date "1995-04-03" @default.
- W2064203216 modified "2023-09-23" @default.
- W2064203216 title "An experimental and computational study of moderately underexpanded rocket exhaust plumes in a co-flowing hypersonic free stream" @default.
- W2064203216 cites W2075553342 @default.
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- W2064203216 doi "https://doi.org/10.2514/6.1995-6127" @default.
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