Adjoint-Based Sensitivity Analysis for Airfoil Flow Control Aiming at Lift-to-Drag Ratio Improvement
Author:
Affiliation:
1. Keio University, Yokohama 223-8522, Japan
2. Japan Aerospace Exploration Agency, Tokyo 181-0015, Japan
Funder
Japan Aerospace Exploration Agency
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060415
Reference25 articles.
1. Aerodynamic technologies to improve aircraft performance
2. Riblets as a Viscous Drag Reduction Technique
3. Direct numerical simulation of spatially developing turbulent boundary layers with uniform blowing or suction
4. Contribution of Reynolds stress distribution to the skin friction in wall-bounded flows
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