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Effect of Yaw on Boundary Layers at High Speeds
H. G. LewJ. B. Fanucci
出版Department of Aeronautical Engineering, Pennsylvania State University, 1956
URLhttp://books.google.com.hk/books?id=ZF0JAQAAMAAJ&hl=&source=gbs_api
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註釋The flow over yawed infinite wings in a compressible fluid have been considered with heat transfer at the surface. The main results are the wall shear, heat transfer coefficient, and the modified Reynolds analogy variations with sweepback.