Measurements of Midspan Flow Interactions of a Low-Aspect-Ratio Circulation Control Wing
Author:
Affiliation:
1. United States Naval Academy, Annapolis, MD 21402
2. Naval Air Systems Command, Patuxent River, MD 20670
3. Naval Sea Systems Command, West Bethesda, MD 20376
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033852
Reference18 articles.
1. Mid-span PIV Measurements of a Low Aspect Ratio Circulation Control Wing
2. RiebeJ. M. “A Correlation of Two-Dimensional Data on Lift Coefficient Available with Blowing- Suction- Slotted- and Plain-Flap High-Lift Devices,” Langley Aeronautical Lab. RM-L55D29a, Langley Field, VA, 1955.
3. STOL - THE POTENTIAL OF THE CIRCULATION CONTROL WING CONCEPT
4. HarrisM. “Investigation of the Circulation Control Wing Upper Surface Blowing High-Lift System on a Low Aspect Ratio Semispan Model,” David W. Taylor Naval Ship Research and Development Center Rept. ASED-81/10, Bethesda, MD, 1981.
5. Investigation of a circular planform wing with tangential fluid ejection
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