Design of a Supersonic Oxy-Methane Combustor for Direct Power Extraction
Author:
Affiliation:
1. University of Texas, El Paso
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0243
Reference29 articles.
1. Numerical Analysis of Reentry Trajectory Coupled with Magnetohydrodynamics Flow Control
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3. Influences of Electrical Conductivity of Wall on Magnetohydrodynamic Control of Aeroynamic Heating
4. Numerical Studies of Magnetohydrodynamic Flow Control Considering Real Wall Electrical Conductivity
5. Numerical Analysis of Reentry Trajectory Coupled with Magnetohydrodynamics Flow Control
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. Heat Transfer Characterization Methodology for an Oxy-Fuel Direct Power Extraction Combustion System;Journal of Propulsion and Power;2018-09
2. Heat Transfer Characterization of a High Heat Flux Oxy-Fuel Direct Power Extraction Combustor;55th AIAA Aerospace Sciences Meeting;2017-01-05
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