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Shock Wave Assessment for High Speed Compressible Flows

Ashish Anand Verma

出版	University of North Carolina at Charlotte, 2007
URL	http://books.google.com.hk/books?id=UWQ-nQEACAAJ&hl=&source=gbs_api

註釋

Shock wave turbulent boundary layer interactions are one of the most complex phenomena in the field of compressible fluid dynamics. Modeling turbulences in supersonic and hypersonic flow, boundary layer separation and oblique shock wave formation are important aspects of such interactions. This present work focuses on assessment of turbulent modeling for such interactions ranging from a fully attached flow to a severely separated flow. The model predictions are compared with experimental data provided by Settles and Dodson using a Princeton Channel. The results provide an understanding of separation of boundary layers with respect to pressure gradients.