Numerical Simulation of a 65-Degree Delta-Wing Flowfield
Author:
Affiliation:
1. U.S. Air Force Wright Laboratory, Wright Patterson Air Force Base, Ohio 45433-7913
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2218
Reference36 articles.
1. Large-amplitude high-rate roll experiments on a delta and double delta wing
2. Prediction of leading-edge vortex breakdown on a delta wing oscillating in roll
3. Body-axis rolling motion critical states of a 65-degree delta wing
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