Prediction of Transonic Buffet Onset for an Airfoil with Shock Induced Separation Bubble Using Steady Navier-Stokes Solver-Reference-Cited by-同舟云学术

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Prediction of Transonic Buffet Onset for an Airfoil with Shock Induced Separation Bubble Using Steady Navier-Stokes Solver

Published:2002-06-24 Issue: Volume: Page:
ISSN:
Container-title:20th AIAA Applied Aerodynamics Conference
language:
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Author:

Chung Injae¹,Lee Duckjoo²,Reu Taekyu¹

Affiliation:

1. Agency for Defense Development

2. Korea Advanced Institute of Science and Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2002-2934

Reference18 articles.

1. Pearcey, H. H. "AMethod for the Prediction of the Onset of Buffeting and Other Separation Effects from Wind-Tunnel Tests on Rigid Models,"AGARDReport223, 1958.

2. Butkewicz, P. J. "On Airflow Separation and Buffet Onset During Fighter Aircraft Maneuvering,"AGARDCP-102, 1972.

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