Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings
Multimission Aircraft Fuel-Burn Minimization via Multipoint Aerostructural Optimization
Multipoint Aerodynamic Shape Optimization Investigations of the Common Research Model Wing
Aerodynamic Shape Optimization Investigations of the Common Research Model Wing Benchmark
Component-Based Geometry Manipulation for Aerodynamic Shape Optimization with Overset Meshes
Buffet-Onset Constraint Formulation for Aerodynamic Shape Optimization
High-fidelity computational modeling and optimization of aircraft configurations have the potential to enable engineers to create more
...Efficient Mesh Generation and Deformation for Aerodynamic Shape Optimization