Disturbance-Level and Roughness-Induced Transition Measurements in a Conical Boundary Layer at Mach 6
26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
2008-01-01
Conference paper
Electronic Resource
English
Disturbance-Level and Transition Measurements in a Conical Boundary Layer at Mach 6
British Library Conference Proceedings | 2008
|Boundary-layer transition at Mach 3.12 with and without single roughness elements
Engineering Index Backfile | 1954
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