The Effect of MHD Energy Bypass on Specific Thrust for Supersonic Turbojet Engine-Reference-Cited by-同舟云学术

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The Effect of MHD Energy Bypass on Specific Thrust for Supersonic Turbojet Engine

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
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Author:

Benyo Theresa¹

Affiliation:

1. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-232

Reference6 articles.

1. 2Litchford, R.J., J.W. Cole, V.A. Bityurin, and J.T. Lineberry, "Thermodynamic Cycle Analysis of Magnetohydrodynamic-Bypass HypersonicAirbreathingEngine", NASA TP-2000-210387.

2. Low-temperature M=3 flow deceleration by Lorentz force

3. Magnetogasdynamic Inlet Power Extraction for a Gas Turbine

Cited by 3 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. Preliminary Experimental Investigation on MHD Power Generation Using Seeded Supersonic Argon Flow as Working Fluid;Chinese Journal of Aeronautics;2011-12

2. Flow Matching Results of an MHD Energy Bypass System on a Supersonic Turbojet Engine using the Numerical Propulsion System Simulation (NPSS) Environment;42nd AIAA Plasmadynamics and Lasers Conference;2011-06-14

3. Initial Flow Matching Results of MHD Energy Bypass on a Supersonic Turbojet Engine Using the Numerical Propulsion System Simulation (NPSS) Environment;41st Plasmadynamics and Lasers Conference;2010-06-28

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