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Aircraft
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title: AIAA Journal of Aircraft
Computation of Aircraft Stability Derivatives Using an Automatic Differentiation Adjoint Approach
Flexible Formulation of Spatial Integration Constraints in Aerodynamic Shape Optimization
Multimodality in Aerodynamic Wing Design Optimization
The application of gradient-based optimization to wing design could potentially reveal revolutionary new wing concepts. Giving the
...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
...DAFoam: An Open-Source Adjoint Framework for Multidisciplinary Design Optimization with OpenFOAM
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
...Sensitivity-Based Geometric Parametrization and Automatic Scaling for Aerodynamic Shape Optimization
Aerodynamic shape optimization has become well established, with designers routinely performing wing and full aircraft optimizations
...Linear Stability-Based Smooth Reynolds-Averaged Navier–Stokes Transition Model for Aerodynamic Flows