Direct Numerical Simulation of Hypersonic Boundary-Layer Transition Over Blunt Leading Edges, Part II: Receptivity to Sound
Meeting; 35th, Aerospace sciences ; 1997 ; Reno; NV
1997-01-01
ALL
Nos 97-0001 to 97-1018 with gaps
Aufsatz (Konferenz)
Englisch
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British Library Conference Proceedings | 1997
|Hypersonic Boundary-Layer Stability over Blunt Leading Edges with Bow-Shock Effects
British Library Conference Proceedings | 1998
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