Supersonic Channel Airfoils for Reduced Drag
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332-0150
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.985
Reference19 articles.
1. Supersonic aircraft drag reduction
2. AERODYNAMIC DESIGN FOR SUPERSONIC SPEEDS
3. Anderson, J. D., Hypersonic and High Temperature Gas Dynamics, McGraw-Hill, New York, 1989, pp.250-300.
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