Domain-Element Method for Aerodynamic Shape Optimization Applied to a Modern Transport Wing

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Metric-Based Mathematical Derivation of Efficient Airfoil Design Variables (2015, methodology): “Conversely, the more general control point-based methods have the advantage of being able to use a hierarchical set of design variables, the number of which can be set by the user depending on the problem, and vary from minor control point position perturbations up to entire groups of control points”