Assessment of thermochemical nonequilibrium and slip effects for Orbital Reentry Experiment (OREX)
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-1859
Reference33 articles.
1. Viscous shock-layer study of thermochemical nonequilibrium
2. 3Yamamoto,Y.and Yoshioka,M."CFD and FEM CoupKngAnalysisofOREX AerothermodynamicFlightData,"AIAAPaper 95-2087,June 1995.
3. 4Moss,J. N.andBird,G.A."Direct SimulationTransitionalFlowforHypersonic Re-entry Conditions,"ProgressinAstronautics and Aeronautics: Thermal Design of Aeroassisted OrbitalVehicles, editedbyH.F. Nelson,Vol.96,1985,pp.113-139.
4. ^Yamamoto,Y.,privatecommunication, AerodynamicsDivision,NationalAerospace Lab.,Tokyo-182,Japan,Dec. 1995.
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