Pitch rate effects on delta wing vortex breakdown
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46998
Reference12 articles.
1. 'LeMay, S. P., Batill, S. M, and Nelson, R. C. "Leading Edge Vortex Dynamics on a Pitching Delta Wing/' AIAA Paper 88-2559, June 1988.
2. Large-amplitude high-rate roll experiments on a delta and double delta wing
3. Flow physics of critical states for rolling delta wings
4. Hysteresis of vortex development and breakdown on an oscillating delta wing
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