A new method of boundary layer correction in the design of supersonic wind tunnel nozzle
22nd Aerospace Sciences Meeting ; 1984 ; Reno , NV , U.S.A.
1984-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Boundary-Layer Studies In A 2-D Supersonic Nozzle For Quiet-Tunnel Applications
British Library Conference Proceedings | 1994
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