暂无分享,去创建一个
A. Martellucci | A. Berkowitz | A. Martellucci | A. Berkowitz | C. Kyriss | C. Kyriss
[1] S. Pate,et al. Supersonic Boundary-Layer Transition: Effects of Roughness and Freestream Disturbances , 1971 .
[2] G. Rushton,et al. Shock tunnel investigation of boundary-layer transition at M equals 5.5. , 1966 .