A numerical methodology for an aeroelastic SBLI flow-Reference-Cited by-同舟云学术

A numerical methodology for an aeroelastic SBLI flow

Published:2000-01-10 Issue: Volume: Page:
ISSN:
Container-title:38th Aerospace Sciences Meeting and Exhibit
language:
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Author:

Wood Brett¹,Loth E.¹,Geubelle P.¹,McIlwain S.¹

Affiliation:

1. Illinois, Univ., Urbana

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-552

Reference16 articles.

1. Study of Passive Control in a Transonic Shock Wave/Boundary-Layer Interaction

2. Laurendeau, E. (1995) "Boundary-Layer Bleed Roughness0022, Ph.D. Dissertation,Dept. of Aeronautics and Astronautics, Universityof Washington, Seattle, WA.

3. Lohner, R., Yang, C., Cebral, J.R., Baum, J.D., Luo, H.Pelessone, D. and Chat-man, C. (1995) "Fluid-Structure Interaction using a Loose Coupling Algorithm and Adaptive Unstructured Grids0022, Computational Fluid Dynamics Review, John Wiley, New York, pp.755-776.

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