Three-Dimensional Large-Scale Aerodynamic Shape Optimization Based on Shape Calculus
Three-Dimensional Large-Scale Aerodynamic Shape Optimization Based on Shape Calculus
Large-scale three-dimensional aerodynamic shape optimization based on the compressible Euler equations is considered. Shape calculus is used to derive an exact surface formulation of the gradients, enabling the computation of shape gradient information for each surface mesh node without having to calculate further mesh sensitivities. Special attention is paid to …