Accurate transonic wave drag prediction using simple physical models
Author:
Affiliation:
1. Messerschmitt-Boelkow-Blohm GmbH, Bremen, West Germany
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1986-512
Reference26 articles.
1. Supercritical Wing Sections II
2. R. Bohning, " Die Wechselwirkung eines smkrechten VerdichtungsstoRes m i t einer turbulenten Grenzschicht an einer gekrijmmten Wand", Habilitation, Universitat (TH) Karlsruhe (1982)
3. R. Bohning, private correspondence (1984)
4. L.T. Chen, J.C. Vassberq, C.C. Peavey, "A Transonic Wing-Body Flowfield Calculation with Improved Grid Topology and Shock-Point Operators, AIAA Paper 84-2157, Aug. 1984
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