A procedure for calculating laminar, transitional and/or turbulent three-dimensional boundary layers including surface curvature effects about arbitrary blunt-nosed bodies
16th Aerospace Sciences Meeting ; 1978 ; Huntsville , AL , U.S.A.
1978-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Approximate Viscous Shock Layer Technique for Calculating Hypersonic Flows About Blunt-Nosed Bodies
Online Contents | 1994
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