Evolution of a 2-D disturbance in a supersonic boundary layer and the generation of shocklets

Author:

Zhang-feng Huang,Heng Zhou

Publisher

Springer Science and Business Media LLC

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials

Reference7 articles.

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Theoretical investigation on shocklets in compressible boundary layers;Applied Mathematics and Mechanics;2014-06-25

2. Shocklets in compressible flows;Applied Mathematics and Mechanics;2013-11-09

3. The effects of variable specific heat on the stability of hypersonic boundary layer on a flat plate;Applied Mathematics and Mechanics;2010-07-24

4. Effect of disturbances at inlet on hypersonic boundary layer transition on a blunt cone at small angle of attack;Applied Mathematics and Mechanics;2010-05

5. Numerical study of a positive displacement blower;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2009-05-22

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