Forebody Slot Blowing on Vortex Breakdown and Load Over a Delta Wing
Author:
Affiliation:
1. National University of Singapore, Singapore 117508, Republic of Singapore
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.34293
Reference42 articles.
1. Peckham, D. H., and Atkinson,S. A. "Preliminary Results of Low Speed Wind Tunnel Tests on a Gothic Wing of Aspect Ratio 1.0," British Aeronautical Research Council CP508, Her Majesty's Stationery Office, London,April 1957, pp.1-37.
2. Vortex Breakdown
3. The Structure of Vortex Breakdown
4. Vortex breakdown: Observations and explanations
5. Aspects of vortex breakdown
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