Detailed modeling of electron emission for transpiration cooling of hypersonic vehicles
Author:
Affiliation:
1. University of Michigan, 1320 Beal Avenue, Ann Arbor, Michigan 48109, USA
2. Texas A & M University, 607 A H.R. Bright Bldg., College Station, Texas 77843, USA
Funder
U.S. Department of Energy (DOE)
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
http://aip.scitation.org/doi/pdf/10.1063/1.4974961
Reference25 articles.
1. Theory of Stagnation Point Heat Transfer in Dissociated Air
2. Generalization of the Far-Field Drag Decomposition Method to Unsteady Flows
3. Thermionic Emission
4. High performance modeling of atmospheric re-entry vehicles
5. A Viscosity Equation for Gas Mixtures
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