LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY
Author:
Affiliation:
1. California Institute of Technology, Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.1644
Reference15 articles.
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