High-Fidelity Aerostructural Optimization with a Geometrically Nonlinear Flutter Constraint
Estimating Flutter Bifurcation Diagrams Using the State Velocity
This paper introduces a method for estimating flutter bifurcation diagrams of systems described by time-domain state-space models. The
...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
...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
...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
...Aeroelastic Stability of Conventional and Tow-Steered Composite Plates Under Stochastic Fiber Volume
Propeller Effects on the Response of High-Altitude Long-Endurance Aircraft
Geometrically Nonlinear Aeroelastic Scaling for Very Flexible Aircraft
X-HALE: A Very Flexible Unmanned Aerial Vehicle for Nonlinear Aeroelastic Tests