Design method with controllable velocity direction at throat for inward-turning inlets
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DOI: 10.1016/j.cja.2019.04.012
Abstract: Abstract In the design of a hypersonic inward-turning inlet by applying the traditional basic flow-field, a reflected shock-wave is formed in the isolator due to the continuous reflection of the cowl-reflected shock wave in the… read more here.
Keywords: basic flow; inward turning; method; flow field ... See more keywords