Asymmetry effects in numerical simulation of supersonic flows with upstream separated regions-Reference-Cited by-同舟云学术

Asymmetry effects in numerical simulation of supersonic flows with upstream separated regions

Published:2001-01-08 Issue: Volume: Page:
ISSN:
Container-title:39th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Rodriquez C.¹

Affiliation:

1. National Research Council, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-84

Reference15 articles.

1. Heiser,W.H.,andPratt,D.T.,Hypersonic Airbreathing Propulsion, AIAAEducationalSeries, 1993.

2. Carroll,B.F. "ANumericalandExperimentalInvestigationofMultipleShockWave/TurbulentBoundary-Layer InteractionsinRectangularDucts",Ph.D.thesis,MechanicalandIndustrialEngineeringDept.,UniversityofIllinois atUrbana-Champaign,Urbana,Illinois, 1988.

3. Characteristics of multiple shock wave/turbulent boundary-layer interactions in rectangular ducts

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