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Reynolds Number Effects on the Induced Pressures of Cylindrical Bodies with Different Nose Shapes and Nose Drag Coefficients in Helium at a Mach Number of 24

Richard D. Wagner (Jr.)Ralph WatsonUnited States. National Aeronautics and Space Administration

出版	National Aeronautics and Space Administration, 1963
URL	http://books.google.com.hk/books?id=F2cZH_NobC4C&hl=&source=gbs_api
EBook	FULL_PUBLIC_DOMAIN

註釋Exact inviscid pressure distributions and shock shapes, obtained by the method of characteristics, are compared with experimental data. The results indicate a strong dependence of induced pressures upon Reynolds number, especially in the region immediately downstream of the nose-cylinder junction. The measured shock shapes revealed no discernible effect of Reynolds number variations.