A study of algebraic and half-equation turbulence models for hypersonic PNS predictions-Reference-Cited by-同舟云学术

A study of algebraic and half-equation turbulence models for hypersonic PNS predictions

Published:1988-01-11 Issue: Volume: Page:
ISSN:
Container-title:26th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

SHIRAZI SIAMACK¹,TRUMAN C.¹

Affiliation:

1. New Mexico, University, Albuquerque

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1988-222

Reference29 articles.

1. Flow.Over Blunt Delta Wings.' AiAA Journal, Vol. 20, 1982. pp. 205-218. k. Kaul, V.K. end Chaussee, 0.5. `AFUAL Parabollred Navier-Stokes Code: 19EJ AFYAL/NASA Merged Baseline Versions.' US Air Force Yright Aeronautica 1 Lab., AFWAL-TR-85-3118. 1983. 5. McUherter. M. Noack. R.Y. and Oberkampf. Y.L. "Evaluation of Boundary-Layer and Parabolized Navier-Stokes Solutions for Re-entry Vehicles.'

2. AIAA Journal of Spacecraft and Rockets, Vol. 23, 4 1986. pp. 78-76.

3. Supersonic Flow Past a Sphere-Cone.' AlAA Paper 87-0544. 1987.

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