Efficient Global Optimization of Vortex Generators on a Supercritical Infinite Wing
Author:
Affiliation:
1. Tohoku University, Sendai 980-8577, Japan
2. Kyunghee University, Yongin 446-701, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C033753
Reference31 articles.
1. Numerical Simulation of Micro Vortex Generators
2. Numerical/experimental study of a wingtip vortex in the near field
3. Two-equation eddy-viscosity turbulence models for engineering applications
4. Separation control by vortex generator devices in a transonic channel flow
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