An approximate viscous shock layer technique for calculating nonequilibrium hypersonic flows about blunt-nosed bodies
30th Aerospace Sciences Meeting and Exhibit ; 1992 ; Reno , NV , U.S.A.
1992-01-01
Conference paper
Electronic Resource
English
Approximate Viscous Shock Layer Technique for Calculating Hypersonic Flows About Blunt-Nosed Bodies
Online Contents | 1994
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