Computation of Aircraft Stability Derivatives Using an Automatic Differentiation Adjoint Approach
Multidisciplinary Design Optimization: A Survey of Architectures
Multidisciplinary design optimization is a field of research that studies the application of numerical optimization techniques to the
...Multimission Aircraft Fuel-Burn Minimization via Multipoint Aerostructural Optimization
Computing Stability Derivatives and Their Gradients for Aerodynamic Shape Optimization
Aerodynamic shape optimization of aircraft configurations often ignores stability considerations. To address this, a method for the
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Aerodynamic Shape Optimization Investigations of the Common Research Model Wing Benchmark
Multipoint Aerodynamic Shape Optimization Investigations of the Common Research Model Wing
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
...Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings
Component-Based Geometry Manipulation for Aerodynamic Shape Optimization with Overset Meshes