Numerical Study of Unsteady Shock Waves in Hypersonic Nozzle Flows
32nd AIAA Fluid Dynamics Conference and Exhibit ; 2002 ; St. Louis , Missouri
01.01.2002
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Numerical Investigation of Shock Wave Process with Application to Hypersonic Nozzle Flows
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