Aerodynamic Characteristics of a Pitching Airfoil Through Pressure-Distortion Correction in Pneumatic Tubing
Author:
Affiliation:
1. Aircraft Development Team, Korean Air R&D Center, Daejeon Metropolitan City 305-811, Republic of Korea
2. Department of Aeronautical Science and Flight Operation, Korea Aerospace University, Goyang City, Gyeonggi-do 412-791, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C031941
Reference26 articles.
1. AERODYNAMICS OF SMALL VEHICLES
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4. Aerodynamic lift at Reynolds numbers below 7 x 10 exp 4
5. Wind tunnel tests of wings at Reynolds numbers below 70 000
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