Date: 2014-12-04 04:51:56Fluid 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 ChinaAdd to Reading ListSource URL: www.itam.nsc.ruDownload Document from Source Website File Size: 599,39 KBShare Document on Facebook
|