Effectiveness of Thermionic Emission for Cooling Hypersonic Vehicle Surfaces
Author:
Affiliation:
1. University of Michigan, Ann Arbor
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-1714
Reference37 articles.
1. Inviscid Hypersonic Flow Over Blunt-Nosed Slender Bodies
2. Hyper-X: Foundation for future hypersonic launch vehicles
3. Electron Transpiration Cooling for Hot Aerospace Surfaces
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