Pages that link to "Item:Q2234550"
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The following pages link to Nonlinear energy sink to enhance the landing gear shimmy performance (Q2234550):
Displaying 11 items.
- State feedback fuzzy adaptive control for active shimmy damping (Q647195) (← links)
- Interaction of torsion and lateral bending in aircraft nose landing gear shimmy (Q1041883) (← links)
- Analytical and numerical investigations on inerter-based NES absorber system with nonlinear damping (Q2092922) (← links)
- On the effectiveness of a rod-like distributed piezoelectric controller in preventing the Hopf bifurcation of the visco-elastic Beck's beam (Q2141527) (← links)
- A study on torsional vibration attenuation in automotive drivetrains using absorbers with smooth and non-smooth nonlinearities (Q2281926) (← links)
- Anti-skid induced aircraft landing gear instability (Q2853540) (← links)
- Dynamic shimmy behavior and bifurcation analysis of driver-vehicle-road system (Q6081814) (← links)
- Control of nonlinear vibration of beams subjected to moving loads using tuned mass dampers (Q6098726) (← links)
- Using nonlinear feedback control to improve aircraft nose landing gear shimmy performance (Q6100373) (← links)
- Torsional vibration suppression of rotor systems using a rubber-based nonlinear energy sink (Q6169743) (← links)
- An enhanced electromagnetic-based nonlinear energy sink for hybrid passive control and energy harvesting from resonant vibrations (Q6544660) (← links)