AIAA 2001-0208 Boundary Layer Transition Measurements in Hypervelocity Flows in a Shock Tunnel
39th, Aerospace sciences meeting ; 2001 ; Reno, NV
2001-01-01
ALL
Paper nos AIAA-2001-0007 to AIAA-2001-0660 with gaps
Conference paper
English
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FLUID DYNAMICS - Boundary-Layer Transition Measurements in Hypervelocity Flows in a Shock Tunnel
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