DAFoam: An Open-Source Adjoint Framework for Multidisciplinary Design Optimization with OpenFOAM
Multimodality in Aerodynamic Wing Design Optimization
Boundary-Layer Ingestion Benefit for the STARC-ABL Concept
Modeling Boundary Layer Ingestion Using a Coupled Aeropropulsive Analysis
Computing Stability Derivatives and Their Gradients for Aerodynamic Shape Optimization
Computation of Aircraft Stability Derivatives Using an Automatic Differentiation Adjoint Approach