Numerical analysis of shock wave and supersonic turbulent boundary interaction between adiabatic and cold walls-Reference-Cited by-同舟云学术

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Numerical analysis of shock wave and supersonic turbulent boundary interaction between adiabatic and cold walls

Published:2017-04-07 Issue:6 Volume:18 Page:569-588
ISSN:1468-5248
Container-title:Journal of Turbulence
language:en
Short-container-title:Journal of Turbulence

Author:

Tong Fulin,Tang Zhigong,Yu Changping,Zhu Xingkun,Li Xinliang

Funder

National Key Research and Development Program of China

National Natural Science Foundation of China

Science Challenge Project

Publisher

Informa UK Limited

Subject

General Physics and Astronomy,Mechanics of Materials,Condensed Matter Physics,Computational Mechanics

Link

https://www.tandfonline.com/doi/pdf/10.1080/14685248.2017.1311017

Reference26 articles.

1. Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow

2. Unsteady wave structure near separation in a Mach 5 compression rampinteraction

3. Turbulence structure in a shock wave/turbulent boundary-layer interaction

4. Direct simulation of the turbulent boundary layer along a compression ramp at M = 3 and Reθ = 1685

5. Direct Numerical Simulation of Supersonic Turbulent Boundary Layer over a Compression Ramp

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3. Wall temperature effects on aerodynamic heating mechanisms in shock wave turbulent boundary layer interaction;AIAA SCITECH 2024 Forum;2024-01-04

4. Direct numerical simulation of compression ramp shock wave/boundary layer interaction controlled by plasma actuator array;Physics of Fluids;2023-12-01

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