Pages that link to "Item:Q5962985"
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The following pages link to Bifurcation analysis of aero-engine's rotor system under constant maneuver load (Q5962985):
Displaying 7 items.
- Nonlinear vibration phenomenon of an aircraft rub-impact rotor system due to hovering flight (Q314316) (← links)
- Bifurcation analysis for 2:1 and 3:1 super-harmonic resonances of an aircraft cracked rotor system due to maneuver load (Q327885) (← links)
- Bifurcation analysis of fan casing under rotating air flow excitation (Q468573) (← links)
- Bifurcation characteristics analysis of a class of nonlinear dynamical systems based on singularity theory (Q1674149) (← links)
- Retardational Effect and Hopf Bifurcations in a New Attitude System of Quad-Rotor Unmanned Aerial Vehicle (Q5008971) (← links)
- Bifurcation Modes of Periodic Solution in a Duffing System Under Constant Force as Well as Harmonic Excitation (Q5206888) (← links)
- Nonlinear dynamics of marine rotor-bearing system coupled with vibration isolation structure subject to ship rolling motion (Q6135590) (← links)