NASA NTRS · 19910016029
A Numerical Study of Hypersonic Forebody/Inlet Integration Problem
Abstract
A numerical study of hypersonic forebody/inlet integration problem is presented in the form of the view-graphs. The following topics are covered: physical/chemical modeling; solution procedure; flow conditions; mass flow rate at inlet face; heating and skin friction loads; 3-D forebogy/inlet integration model; and sensitivity studies.
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Kumar, Ajay. 1991-01-10. A Numerical Study of Hypersonic Forebody/Inlet Integration Problem. https://ntrs.nasa.gov/citations/19910016029
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