AXISYMMETRIC TURBULENT SHOCKWAVE BOUNDARY LAYER INTERACTION AT MACH 2.5
AIAA Aviation Forum ; 2020 ; Online
Fluid dynamics ; Volume 2 of 3 ; 1106-1125
2020
Conference paper
English
Flow Field Measurements in a Crossing Shockwave Turbulent Boundary Layer Interaction at Mach 3
British Library Conference Proceedings | 1993
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