Experiment on Shock Layer Enhancement by Electro-Magnetic Effect in Reentry-Related High-Enthalpy Flow
Author:
Affiliation:
1. University of Tokyo
2. Japan Aerospace Exploration Agency
3. EADS
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-4786
Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Effect of the Shape Variation on the Electrodynamic Heat Shield System under the Strong Magnetic Field;44th AIAA Plasmadynamics and Lasers Conference;2013-06-22
2. Effect of the Strong Magnetic Field on the Electrodynamic Heat Shield System for Reentry Vehicles;43rd AIAA Plasmadynamics and Lasers Conference;2012-06-25
3. Impact of Lift Force by Electromagnetic Flow Control on the Reentry Trajectory;42nd AIAA Plasmadynamics and Lasers Conference;2011-06-14
4. Effect of the nose bluntness on the electromagnetic flow control for reentry vehicles;Shock Waves;2009
5. Application of the Magnetic Flow Control System for Aerobraking Flight of the Reentry Vehicle;39th Plasmadynamics and Lasers Conference;2008-06-15
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