Numerical investigation of evolution of disturbances in supersonic sharp cone boundary layers
Author:
Publisher
Springer Science and Business Media LLC
Subject
Applied Mathematics,Mechanical Engineering,Mechanics of Materials
Link
http://link.springer.com/content/pdf/10.1007/s10483-006-0601-1.pdf
Reference3 articles.
1. Poinsot T J, Lele S K. Boundary conditions for direct simulations of compressible viscous flows[J]. Journal of Computational Physics, 1992, 101(1):104–129.
2. Huang Zhangfeng, Zhou Heng. Evolution of a 2-D disturbance in a supersonic boundary layer and the generation of shocklets[J]. Applied Mathematics and Mechanics (English Edition), 2004, 25(1):1–9.
3. Cao Wei, Zhou Heng. A numerical investigation of the evolution of 2-D disturbances in hypersonic boundary layers and the effect on the flow structure due to the existence of shocklets[J]. Science in China, Ser G, 2004, 47(2):244–255.
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