An interactive boundary-layer method for multielement airfoils-Reference-Cited by-同舟云学术

An interactive boundary-layer method for multielement airfoils

Published:1998-06 Issue:5-6 Volume:27 Page:651-661
ISSN:0045-7930
Container-title:Computers & Fluids
language:en
Short-container-title:Computers & Fluids

Author:

Cebeci Tuncer,Besnard Eric,Chen Hsun H.

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference14 articles.

1. Rogers, S. E., Wiltberger, N. L. and Kwak, D., Efficient simulation of incompressible viscous flow over single- and multielement airfoils. AIAA Paper No. 92-0405, 1992

2. Rogers, S. E. Progress in high-lift aerodynamic calculations. AIAA Paper No. 93-0194, January 1993

3. Valarezo, W. O. and Mavriplis, D. J. Navier–Stokes applications to high-lift airfoil analysis. AIAA Paper No. 93-3534, August 1993

4. Cebeci, T., Calculation of multielement airfoils and wings at high lift. In AGARD Conference Proceedings 515 on High-Lift Aerodynamics, Paper No. 24, Banff, Alberta, Canada, October 1992

5. Cebeci, T., Besnard, E. and Messié, S., A stability/transition-interactive-boundary-layer approach to multielement wings at high lift. AIAA Paper No. 94-0292, January 1994

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