NASA NTRS · 20030053190
Profile Optimization Method for Robust Airfoil Shape Optimization in Viscous Flow
Abstract
Simulation results obtained by using FUN2D for robust airfoil shape optimization in transonic viscous flow are included to show the potential of the profile optimization method for generating fairly smooth optimal airfoils with no off-design performance degradation.
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Li, Wu. 2003-05-01. Profile Optimization Method for Robust Airfoil Shape Optimization in Viscous Flow. https://ntrs.nasa.gov/citations/20030053190
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