Computation of Aircraft Stability Derivatives Using an Automatic Differentiation Adjoint Approach
X-HALE: A Very Flexible Unmanned Aerial Vehicle for Nonlinear Aeroelastic Tests
Reduced-Order Modeling Approach for Blisks with Large Mass, Stiffness, and Geometric Mistuning
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
...Geometrically Nonlinear Aeroelastic Scaling for Very Flexible Aircraft
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