Numerical Simulation of Supersonic MHD Channel Flows-Reference-Cited by-同舟云学术

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Numerical Simulation of Supersonic MHD Channel Flows

Published:2006-06-05 Issue: Volume: Page:
ISSN:
Container-title:9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference
language:
Short-container-title:

Author:

Xu Zhenyu¹,Lee Chun-Hian²,Amano Ryo¹

Affiliation:

1. University of Wisconsin-Milwaukee

2. Beihang University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2941

Reference13 articles.

1. 1GurijianovEP,HarshaPT."AJAXNewdirectionsinhypersonictechnology",AIAApaper2000-0614, 2000

2. 2ClaudioB,PaulAC."Anelectro-magnetic-chemicalhypersonicpropulsionsystem",AIAApaper98-1582, 1998

3. 3ChaseRL,BoydR,CzyszP,FroningHD,LewisM,MckineeyLE."AnAJAXtechnologyforadvanced SSTO designconcept", AIAApaper98-5527,1998

4. 4BrichkinDI,KuranovAL,SheikinEG."MHD-technologyforscramjetcontrol",AIAApaper98-1642, 1998

5. 5GaitondeDV,PoggieJ."SimulationofMHDflowcontroltechniques",AIAApaper2000-2326,2000

Cited by 1 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. Edge-Based Finite Element Modeling of Magnetogasdynamic-Based Propulsion Systems;AIAA Journal;2019-07

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