Experimental and Numerical Investigation of 65 Degree Delta and 65/40 Degree Double-Delta Wings
Author:
Affiliation:
1. King Fahd University of Petroleum and Minerals, Dhahran 31261, Saudi Arabia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.20243
Reference39 articles.
1. Aerodynamic Performance of Delta Wings at Supersonic Speeds
2. Predictions of vortex-lift characteristics by a leading-edge suctionanalogy
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