Aerodynamic Shape Optimization Investigations of the Common Research Model Wing Benchmark
Aeroelastic Stability of Conventional and Tow-Steered Composite Plates Under Stochastic Fiber Volume
Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings
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
...Component-Based Geometry Manipulation for Aerodynamic Shape Optimization with Overset Meshes
Computation of Aircraft Stability Derivatives Using an Automatic Differentiation Adjoint Approach
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
...Coupled Newton–Krylov Time-Spectral Solver for Flutter and Limit Cycle Oscillation Prediction
Flutter and limit cycle oscillation (LCO) are important phenomena that need to be considered in aircraft design. Previous harmonic
...DAFoam: An Open-Source Adjoint Framework for Multidisciplinary Design Optimization with OpenFOAM
Data-Driven Forecasting of Postflutter Responses of Geometrically Nonlinear Wings
Ensuring adequate flutter margins is a critical step in aircraft design. However, in the presence of nonlinear effects, subcritical
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