Numerical Simulation of Half-Span Aircraft Model with High-Lift Devices in Wind Tunnel
Author:
Affiliation:
1. Japan Aerospace Exploration Agency
2. Ryoyu Systems Company, Ltd.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-333
Reference40 articles.
1. The aerodynamic design of multi-element high-lift systems for transport airplanes
2. Prediction of high lift: review of present CFD capability
3. Johnson, P., Jones, K. M., and Madson, M. "Experimental Investigation of a Simplified 3D High Lift Configuration in Supportof CFDValidation,"AIAAPaper2000-4217,Aug.2000.
4. Rogers, S.E., Roth, K., and Nash, S. M. "CFD Validation of High-Lift Flows with Significant Wind-Tunnel Effects," AIAA Paper 2000-4218,Aug.2000.
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