Aerodynamic design and optimization in one shot
Author:
Affiliation:
1. Weizmann Institute of Science, Rehovot, Israel; ICASE, Hampton, VA
2. Vigyan, Inc., Hampton, VA
3. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-25
Reference18 articles.
1. A Theory of Supercritical Wing Sections, with Computer Programs and Examples
2. 4J. L. Stegerand.I.M.Klineberg.AFiniteDifference Method for Transonic Airfoil Design.AIM J., Vol./ I , No. 5, May 1973,pp. 628435.
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