Investigation of Hypersonic Gap Flow of a Reentry Nosecap with Consideration of Fluid Structure Interaction (AIAA 2006-0188)
44th, Aerospace sciences meeting: a collection of technical papers; Vol 4 ; 2006 ; Reno, NV
2006-01-01
13 pages
Vol 4 of 23. See also m06/23197 � m06/23220
Conference paper
English
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AIAA 2006-0582 Hypersonic Reentry Vehicle Wake Flow Fields at Angle of Attack
British Library Conference Proceedings | 2006
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