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L/D CL = 1 : maximized CL_max : maximized dCL_max : minimized Participating solvers: XFOIL. L/D CL = 1 : maximized CL_max : maximized Participating solvers: XFOIL. While there has been some research dedicated to RANS-
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From a circle to an airfoil via aerodynamic design optimization
The Magic of Optimization: From a Random Generated Surface to a Smooth and Optimized Wing
Aerodynamic Shape Optimization of the ONERA M6 Wing
Aerodynamic shape optimization starting from random initial geometry
CRM Wing Optimization with 100% Thickness Constraint
Introduction to Optimization . Part 3 - Gradient-Based Optimization
Introduction To Optimization: Gradient Based Algorithms
Multipoint aerodynamic shape optimization of the CRM Wing
RANS-based Aerodynamic Shape Optimization of the Blended Wing Body Aircraft
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Last Updated: June 13, 2026
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