Edge-Based Finite Element Modeling of Magnetogasdynamic-Based Propulsion Systems-Reference-Cited by-同舟云学术

Edge-Based Finite Element Modeling of Magnetogasdynamic-Based Propulsion Systems

Published:2019-07 Issue:7 Volume:57 Page:3003-3013
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Zhang Wenbo,Habashi Wagdi G.,Salah Nizar Ben¹,Isola Dario,Baruzzi Guido S.

Affiliation:

1. École nationale supérieure d'ingénieurs de Tunis, Tunis 1008, Tunisia

Funder

Lockheed Martin

Natural Sciences and Engineering Research Council of Canada

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference29 articles.

1. Ben SalahN. “A Finite Element Method for the Fully-Coupled Magnetohydrodynamics,” Ph.D. Thesis, Concordia Univ., Montreal, 1999, https://spectrum.library.concordia.ca/903/ [retrieved 2019].

2. ParkC.BogdanoffD.MehtaU. “Theoretical Performance of a Nonequilibrium MHD Bypass Scramjet,” AIAA Paper 2001-0792, Jan. 2001. doi:10.2514/2.6156

3. Numerical Simulation of Supersonic MHD Channel Flows

4. Flow Simulations within Strong Magnetic Fields

5. Numerical Simulation of Aerodynamic Flow Including Induced Magnetic and Electric Fields

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