Computation of Flow over a High Performance Parafoil
Author:
Affiliation:
1. California State University, Northridge
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2979
Reference10 articles.
1. 2Burk, S. M. and Ware, G. M. "Static Aerodynamic Characteristics of Three Ram-Air Inflated Low Aspect Ratio Wings," NASA TN-D-4182,1967.
2. A review of para-foil applications
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