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Flugmechanik
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High-fidelity Modeling and Simulation of Flutter/LCO for All-movable Horizontal Tail with Free-play
Unsteady Aeroelasticity of Generic Transport Model
Mixed Newtonian-Lagrangian Approach for the Analysis of Flexible Aircraft Dynamics
Effects of Articulated Wings on the Stability of Small Unmanned Aircraft
Linear, Parameter Varying Model Reduction for Aeroservoelastic Systems
An Initial Flight Investigation of Formation Flight for Drag Reduction on the C-17 Aircraft
Numerical Continuation Analysis of a Dual-Sidestay Main Landing Gear Mechanism
Using Indirect Turbulence Measurements for Real-Time Parameter Estimation in Turbulent Air
Guidance algorithms for proximity to target spacecraft
Effect Of Jump Strut Nose Landing Gear In Preliminary Design Of Aircraft
Bifurcation Analysis of a Coupled Nose Landing Gear-Fuselage System
A Conceptual Study of Airfoil Performance Enhancement Using CFD
Bifurcation Analysis of the Generic Transport Model with a View to Upset Recovery
Method for Analyzing The Influence of Random Factors in Carrier Launching
Real-Time Frequency Response Estimation Using Multi-Sine Inputs and Recursive Fourier Transform
Towards Industrialisation of Bifurcation Analysis in Rotorcraft Aeroelastic Problems