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Fluid mechanics / Airspeed / Spacecraft propulsion / Hypersonic speed / Mach number / Hypersonic wind tunnel / Oblique shock / Shock wave / Wind tunnel / Aerodynamics / Aerospace engineering / Fluid dynamics


ICMARTEST OF FORCED BOUNDARY-LAYER TRANSITION ON HYPERSONIC INLET H. Zhao, M. Yi, H. Ni, W. Liu China Aerodynamics Research and Development Center, Mianyang, Sichuan, People’s Republic of China
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Document Date: 2014-12-04 04:51:56

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