Numerical Solution of Three-Dimensional Unsteady Transonic Flow over Swept Wings
Author:
Affiliation:
1. Boeing Military Airplane Company, Seattle, Wash.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.51079
Reference25 articles.
1. Inviscid transonic flow over airfoils
2. 2Magnus, R. J. and Yoshihara, H. "Unsteady Transonic Flows Over an Airfoil,'M/y4L4 Journal, Vol.13, Dec.1975, pp.1622-1628.
3. 3Murman, E. M. and Cole, J. D. "Calculation of Plane Steady Transonic Flows,'M/A4 Journal, Vol.9, Jan. 1971, pp.114-121.
4. 4Ballhaus, W. F. and Bailey, F. R. "Numerical.Calculation of Transonic Flow About Swept Wing/' AIAA Paper 72-677, June 1972.
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