Euler solutions of transonic vortex flows around the Dillner wing - Compared and analyzed
Author:
Affiliation:
1. Flygtekniska Forsoksanstalten, Bromma, Sweden
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1984-2142
Reference9 articles.
1. Three Dimensions, AGARD CP-No. 342, Paris 1983. 2 Fluid Dynamics Panel Working Group 07.
2. to Compute Transonic Flow Around Wing-Body Combinations, =. Vol. 20, pp.1321-1328, Oct 1982. 4 Rizzi,A.W. and Eriksson, L.E.: Compu
3. ation and Computer-Aided Analysis of Mesh Effects, Doctoral dissertation,Uppsala Univ., March 1984. 10 Miller, D.S. and Wood,R.M.: An Investi
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2. Computation of Vortex Flow on a Delta Wing at Transonic Speed;Symposium Transsonicum III;1989
3. Flat plate delta wing separated flows with zero total pressure losses;25th AIAA Aerospace Sciences Meeting;1987-03-24
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