Aerodynamic Shape Optimization Based on Free-form Deformation

By J. Samareh. 2004

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Expected drag minimization for aerodynamic design optimization based on aircraft operational data (2017, background): “The first adjoint-based investigations focused on drag minimization at a single flight condition [2, 33, 37, 39].”
Metric-Based Mathematical Derivation of Efficient Airfoil Design Variables (2015, methodology): “Surface Representation and Perturbation Within the aerodynamic shape optimization process, the problems of geometry representation and perturbation, and the required surface and volume mesh deformations if using a CFD code, can be considered separate problems, though unified approaches are becoming ”
Universal Parametric Geometry Representation Method (2008, methodology): “Numerous methods [2–8] have been devised to numerically represent class 1 airfoil type geometries for use in aerodynamic design, optimization, and parametric studies.”