Modelling catalytic recombination heating at hypersonic speeds-Reference-Cited by-同舟云学术

Modelling catalytic recombination heating at hypersonic speeds

Published:1989-01-09 Issue: Volume: Page:
ISSN:
Container-title:27th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

BRUNO CLAUDIO¹

Affiliation:

1. Roma, Universita, Rome, Italy

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1989-309

Reference59 articles.

1. Aerothermodynamic heating and performance analysis of a high-lift aeromaneuvering AOTV concept

2. Theory of Stagnation Point Heat Transfer in Dissociated Air

3. Curry, M.C., Rochelle, W.C., Chao, D.C., and Ting,P.C. "SpaceShuttleOrbiterNose CapThermal Analysis", AIAA Paper 86-0388 presented at AIAA24thAerospaceSciencesMeeting,Reno,Nevada,January 6-9,1986.

4. Scott, C.D. "Space Shuttle Laminar Heating withFiniteRateCatalyticRecombination",in: ProgressinAstronautics and Aeronautics, Vol.82,ed. byT.E. Horton,AIAA, New York, 1982,pp.248-272.

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