Hypersonic Magneto-Fluid-Dynamic Compression in Cylindrical Inlet-Reference-Cited by-同舟云学术

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Hypersonic Magneto-Fluid-Dynamic Compression in Cylindrical Inlet

Published:2007-06-15 Issue: Volume: Page:
ISSN:
Container-title:38th Plasmadynamics and Lasers Conference
language:
Short-container-title:

Author:

Shang Joseph¹,Chang C.²

Affiliation:

1. Wright State University

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-3885

Reference25 articles.

1. Murthy,S.N.B. and Curran, E.T.,HighSpeed FlightPropulsionSystems, Progress inAeronautics and Astronautics,Vol. 137,AIAA,1991.

2. Kurth, G., Critical Physical Phenomena inScramjet Propulsion,AGARD-CP-600,2002,pp. C5.1- C5.11.

3. Bityurin,V.,Kilmov, A.,Leonov,S., Lutsky, A,VanWieD.,Brovkin,V., and Kolesnichenko,Yu., Effect ofHetrogenousDischargePlasma on ShockWave Structureand Propagation,AIAA99-4940,NorfolkVA, Nov.

Cited by 2 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. Investigation of plasma–surface interaction effects on pulsed electrostatic manipulation for reentry blackout alleviation;Journal of Physics D: Applied Physics;2017-02-09

2. Flow Control Using Thermal Bumps in Hypersonic Flow;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04

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