X-HALE: A Very Flexible Unmanned Aerial Vehicle for Nonlinear Aeroelastic Tests
On the Applicability of an Unsteady Aerodynamic ROM to the Transonic Flight Regime
Reduced-Order Modeling of Hypersonic Vehicle Unsteady Aerodynamics
Structural Models for Flight Dynamic Analysis of Very Flexible Aircraft
Nonlinear Aeroelasticity of a Very Flexible Blended-Wing-Body Aircraft
A Reduced Order Modeling Framework for Integrated Thermo-Elastic Analysis of Hypersonic Vehicles
PROPELLER INFLUENCE ON THE STABILITY OF HALE AIRCRAFT
Gust Load Alleviation Control for Very Flexible Aircraft
Effect of Control Surface-Fuselage Inertial Coupling on Hypersonic Vehicle Flight Dynamics
AIAA-2004-2038 Reduced Structural Modeling of Integrally-Strained Slender Wings
IMPLEMENTATION AND FLIGHT TESTING OF AN ENHANCED STABILITY SYSTEM FOR A VERY FLEXIBLE AIRCRAFT
AIAA-2004-1654 A Framework for Morphing Capability Assessment
Reduced-Order Aerothermoelastic Framework for Hypersonic Vehicle Control Simulation