Wing and conical body of arbitrary cross section in supersonic flow
Author:
Affiliation:
1. McGill University, Montreal, Quebec, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45432
Reference25 articles.
1. 2Carafoli, E., Mateescu, D., and Nastase, A., Wing Theory in Supersonic Flow, Pergamon Press, New York, 1969, pp.27-107.
2. 5Ward, G. N., Linearized Theory of Steady High-Speed Flow, Cambridge University Press, London 1955, pp.135-164.
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