Flow-around airfoils with blunt, round, and sharp trailing edges
Author:
Affiliation:
1. Scientific Research Associates, Inc., Glastonbury, Connecticut
2. Imperial College of Science and Technology, London, England, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45568
Reference24 articles.
1. Reduction of base drag
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