Euler solutions for transonic flow past a fighter wing-Reference-Cited by-同舟云学术

Euler solutions for transonic flow past a fighter wing

Published:1987-01 Issue:1 Volume:24 Page:10-16
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Sankar L. N.¹,Malone J. B.²,Schuster D.²

Affiliation:

1. Georgia Institute of Technology, Atlanta, Georgia

2. Lockheed Georgia Company, Marietta, Georgia

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.45404

Reference11 articles.

1. Jameson, A. and Baker, T. J. "Multigrid Solutions of the Euler Equations for Aircraft Configurations," AIAA Paper 84-0093.

2. 2Agarwal, R. K. and Deese, J. E. "Computation of Transonic Viscous Airfoil, Inlet and Wing Flow Fields," AIAA Paper 84-1551.

3. 3Holst, T. L., Kaynak, U., Gundy, K. L., Thomas, S. D., and Flores, J. "Numerical Solution of Transonic Wing Flow Fields Using an Euler/Navier-Stokes Zonal Approach," AIAA Paper 85-1640.

4. 5Borland, C. J. and Sotomayer, W. A. "An Algorithm for Unsteady Transonic Flow about Tapered Wings," AIAA Paper 84-1567.

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