AIAA 2006-0902 Numerical Investigation of Flow Control Mechanisms for Drag Reduction in Supersonic Base-Flows
44th, Aerospace sciences meeting ; 2006 ; Reno, NV
Aerospace sciences meeting ; 10775-10784
2006-01-01
10 pages
VOL 15 of 24 VOLS
Aufsatz (Konferenz)
Englisch
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Numerical Investigation of Transitional Supersonic Base Flows with Flow Control (AIAA 2006-0479)
British Library Conference Proceedings | 2006
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Online Contents | 2007
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