Disturbance-Level and Roughness-Induced Transition Measurements in a Conical Boundary Layer at Mach 6
26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
01.01.2008
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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
|