Magnetohydrodynamic Control of a Hypersonic Shock–Turbulent Boundary Layer Interaction-Reference-Cited by-同舟云学术

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Magnetohydrodynamic Control of a Hypersonic Shock–Turbulent Boundary Layer Interaction

Published:2024-05 Issue:3 Volume:37 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Luo Shichao¹,Wu Liyin²,Chang Yu²

Affiliation:

1. Ph.D. Research Scholar, Hypervelocity Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China (corresponding author).

2. Professor, Hypervelocity Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China.

Publisher

American Society of Civil Engineers (ASCE)

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-4847

Reference25 articles.

1. Control of separated flow in a reflected shock interaction using a magnetically-accelerated surface discharge

2. Bobashev S. V. N. P. Mende and V. A. Sakharov. 2003. “MHD control of the separation phenomenon in a supersonic xenon plasma flow.” In Proc. AIAA Paper No. 2003-168. Reston VA: American Institute of Aeronautics and Astronautics.

3. Modified One-Equation Turbulence Models for Turbulent Magnetohydrodynamic Flows

4. Turbulent hypersonic flow at a wedge-compression corner

5. Numerical Study of Magnetohydrodynamic Flow Control Along Superorbital Reentry Trajectories

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