Theoretical investigation on shocklets in compressible boundary layers

Author:

Yuan Xiang-jiang,Liu Zhi-yong,Shen Qing,Li Guo-liang

Publisher

Springer Science and Business Media LLC

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials

Reference11 articles.

1. Fu, D. X. and Ma, Y. W. Methods of group velocity controlling and numerical simulation of threedimensional planar mixing layer. Proceedings of Modern Mechanics and Science and Technology Progress Conference, China Academy of Mechanics, Beijing, 533–538 (1997)

2. Yuan, X. J. and Zhou, H. A numerical study for small amplitude T-S waves in a supersonic boundary layer. Applied Mathematics and Mechanics (English Edition), 21(12), 1211–1214 (2000) DOI 10.1007/BF02459212

3. Shen, Q., Zhang, H. X., and Yuan, X. J. Numerical simulation of shock-lets within the supersonic boundary layer. Acta Aerodynamica Sinica, 18, 103–108 (2000)

4. Huang, Z. F. and Zhou, H. Evolution of a 2-D disturbance in a supersonic boundary layer and the generation of shocklets. Applied Mathematics and Mechanics (English Edition), 25(1), 1–8 (2004) DOI 10.1007/BF02437288

5. Cao, W. and Zhou, H. 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. Science in China (Series G), 47(2), 244–255 (2004)

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