Effects of Mach Number and Specific Heat Ratio on Low-Reynolds-Number Airfoil Flows
Author:
Affiliation:
1. Department of Space Flight System, Japan Aerospace Exploration Agency, 252-5210 Sagamihara, Japan
2. Department of Aerospace Engineering, Tohoku University, 980-8579 Miyagi, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053468
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4. Aerodynamic lift at Reynolds numbers below 7 x 10 exp 4
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