Flow Control Mechanism Based on Magnetic Induced Vortex for Reentry Vehicles-Reference-Cited by-同舟云学术

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Flow Control Mechanism Based on Magnetic Induced Vortex for Reentry Vehicles

Published:2021-07 Issue:4 Volume:58 Page:1120-1137
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Wang Ding¹^ORCID,Wang Jiang-feng¹,Li Long-fei¹,Yang Tian-peng¹

Affiliation:

1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China

Funder

National Numerical Wind Tunnel Project of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A34918

Reference41 articles.

1. Magnetohydrodynamic Flow Control of a Hypersonic Cruise Vehicle Based on AJAX Concept

2. Surface plasma actuators modeling for flow control

3. Computational Study of Impregnated Ablator for Improved Magnetohydrodynamic Heat Shield

4. Numerical Simulation of MHD Flow Control along Super Orbital Reentry Trajectory

5. Numerical Simulation of control of plasma flow with magnetic field for thermal protection in Earth reentry flight

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1. Study of Two-Fluid Effects in Weakly Ionized Plasma Under Electromagnetic Fields;AIAA Journal;2024-04

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