Experimental Investigation of the Hypersonic Boundary Layer Transition on a 45° Swept Flat Plate-Reference-Cited by-同舟云学术

Experimental Investigation of the Hypersonic Boundary Layer Transition on a 45° Swept Flat Plate

Published:2020-01 Issue:1 Volume:55 Page:111-120
ISSN:0015-4628
Container-title:Fluid Dynamics
language:en
Short-container-title:Fluid Dyn

Author:

Lu Xiaoge,Yi Shihe,He Lin,Liu Xiaolin,Niu Haibo

Publisher

Pleiades Publishing Ltd

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering

Link

http://link.springer.com/content/pdf/10.1134/S0015462820010085.pdf

Reference25 articles.

1. X. L. Liu, S. H. Yi, H. B. Niu, and X. G. Lu, “Influence of laser-generated perturbations on hypersonic boundary-layer stability,” Acta Phys. Sin. 67(2018).

2. X. L. Zhong, “Direct numerical simulation of 3-D hypersonic boundary layer receptivity to freestream disturbances,” The 36th AIAA Aerospace Sciences Meeting and Exhibit, ed: American Institute of Aeronautics and Astronautics, 1998.

3. M. V. Morkovin, E. Reshotko, and T. Herbert, “Transition in open flow systems: a reassessment,” Bull. APS, 39, 31 (1994).

4. Y. J. Wu, X. Ming, “Experimental Study of Initial Disturbance Growth for Cross Flow Instability,” ACTA Aerodynamica Sinica, vol. 18, 2000.

5. S. X. Li, J. K. Ma, and X. G. Guo, “Experimental Study of Hypersonic Interaction Flow Induced by High Sweep Fin Model,” Physics of Gases, vol. 1, 2016.

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