Mixing Enhancement of Compressible Planar Mixing Layer Impinged by Oblique Shock Waves-Reference-Cited by-同舟云学术

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Mixing Enhancement of Compressible Planar Mixing Layer Impinged by Oblique Shock Waves

Published:2015-01 Issue:1 Volume:31 Page:156-169
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Zhang Yunlong¹,Wang Bing¹,Zhang Huiqiang¹,Xue Shuyan¹

Affiliation:

1. School of Aerospace, Tsinghua University, 100084 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35423

Reference46 articles.

1. Large-scale structure and entrainment in the supersonic mixing layer

2. HallJ. L.DimotakisP. E.RosemannH. “Some Measurement of Molecular Mixing in Compressible Turbulent Shear Layers,” AIAA Paper 1991-1719, 1991.

3. Compressibility effects in free shear layers

4. Turbulent shear-layer mixing: growth-rate compressibility scaling

5. Historical Survey on Enhanced Mixing in Scramjet Engines

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