Loop-Separation Control for Very Flexible Aircraft
In this research, a loop-separation concept (LSC) is applied to a very flexible aircraft. Appealing features of this control
...Flexible Aircraft Simulation Validation with Flight Test Data
The challenges of modeling flexible aircraft include appropriate fidelity capturing and validation with experimental data. In fact, the
...Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings
Propeller Effects on the Response of High-Altitude Long-Endurance Aircraft
Geometrically Nonlinear Aeroelastic Scaling for Very Flexible Aircraft
Multimission Aircraft Fuel-Burn Minimization via Multipoint Aerostructural Optimization
Computation of Aircraft Stability Derivatives Using an Automatic Differentiation Adjoint Approach
Flexible Formulation of Spatial Integration Constraints in Aerodynamic Shape Optimization
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
...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
...Multimodality in Aerodynamic Wing Design Optimization
The application of gradient-based optimization to wing design could potentially reveal revolutionary new wing concepts. Giving the
...High-Fidelity Aerostructural Optimization with a Geometrically Nonlinear Flutter Constraint
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
...
Multipoint Aerodynamic Shape Optimization Investigations of the Common Research Model Wing
X-HALE: A Very Flexible Unmanned Aerial Vehicle for Nonlinear Aeroelastic Tests
Aeroelastic Stability of Conventional and Tow-Steered Composite Plates Under Stochastic Fiber Volume
Aerodynamic Shape Optimization Investigations of the Common Research Model Wing Benchmark
DAFoam: An Open-Source Adjoint Framework for Multidisciplinary Design Optimization with OpenFOAM