Prediction of aerothermal characteristics of a generic hypersonic inlet flow
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DOI: 10.1007/s00162-021-00587-7
Abstract: Accurate prediction of aerothermal surface loading is of paramount importance for the design of high-speed flight vehicles. In this work, we consider the numerical solution of hypersonic flow over a double-finned geometry, representative of the… read more here.
Keywords: inlet; prediction aerothermal; aerothermal characteristics; boundary layer ... See more keywords