Impact of angle of attack on plasma flow and electromagnetic wave propagation around hypersonic vehicles-Reference-Cited by-同舟云学术

Impact of angle of attack on plasma flow and electromagnetic wave propagation around hypersonic vehicles

Published:2020-06 Issue:6 Volume:62 Page:2270-2280
ISSN:0895-2477
Container-title:Microwave and Optical Technology Letters
language:en
Short-container-title:Microw Opt Technol Lett

Author:

Ouyang Wenchong¹^ORCID,Liu Yanming¹,Zhang Xu¹

Affiliation:

1. Key Laboratory of Information and Structure Efficiency in Extreme Environment, Ministry of Education of China, School of Aerospace Science and TechnologyXidian University China

Funder

National Natural Science Foundation of China

Publisher

Wiley

Subject

Electrical and Electronic Engineering,Condensed Matter Physics,Atomic and Molecular Physics, and Optics,Electronic, Optical and Magnetic Materials

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/mop.32326

Reference26 articles.

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3. E. D.Gillman J. E.Foster I. M.Blankson. Review of leading approaches for mitigating hypersonic vehicle communications blackout and a method of ceramic particulate injection via cathode spot arcs for blackout mitigation. NASA TM‐2010–216220; 2010.

4. Electromagnetic Reduction of Plasma Density During Atmospheric Reentry and Hypersonic Flights

5. J. W.Meyer Lockheed Martin Corp Palo Alto CA U.S. Patent for System and Method For Reducing Plasma Induced Communication Disruption Utilizing Electrophilic Injection and Sharp Reentry Vehicle Nose Shaping Publication No. US7237752 B1 filed May 18 2004.

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