Fence-induced transition data simulating a raised gap filler have been acquired on the wing lower surface of a Shuttle Orbiter model in the Langley 31-Inch Mach 10 Tunnel to compare with the Shuttle Boundary Layer Transition Flight and HYTHIRM Experiments, and to provide additional correlation data for the Boundary Layer Transition Tool. In a qualitative assessment, the data exhibit the expected response to all parameter variations; however, it is unclear whether fully effective tripping at the fence was ever realized at any test condition with the present model hardware. A preliminary, qualitative comparison of the ground-based transition measurements with those obtained from the STS-128 HYTHIRM imagery at Mach 15 reveal similar transition-wake response characteristics in terms of the spreading and the path along the vehicle surface.
Transition Induced by Fence Geometrics on Shuttle Orbiter at Mach 10
48th AIAA Aerospace Sciences Meeting ; 2010 ; Orlando, FL, United States
2010-01-04
Aufsatz (Konferenz)
Keine Angabe
Englisch
TRANSITION INDUCED BY FENCE GEOMETRIES ON SHUTTLE ORBITER AT MACH 10
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