Pages that link to "Item:Q314316"
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The following pages link to Nonlinear vibration phenomenon of an aircraft rub-impact rotor system due to hovering flight (Q314316):
Displaying 11 items.
- Bifurcation analysis for 2:1 and 3:1 super-harmonic resonances of an aircraft cracked rotor system due to maneuver load (Q327885) (← links)
- Post-critical analysis of ground resonance phenomenon: effect of stator asymmetry (Q331216) (← links)
- Analysis on the nonlinear response of cracked rotor in hover flight (Q623867) (← links)
- Instability zones for isotropic and anisotropic multibladed rotor configurations (Q634937) (← links)
- Analysis of the rub-impact forces between a controlled nonlinear rotating shaft system and the electromagnet pole legs (Q823505) (← links)
- Study on dynamic behaviors of rotor model with coupling faults and applications of TPOD method (Q2089138) (← links)
- Effect of gravity-induced asymmetry on the nonlinear vibration of an overhung rotor (Q2207881) (← links)
- Parametric instability of flexible rotor-bearing system under time-periodic base angular motions (Q2282917) (← links)
- Influence of structural backlash and friction in command system on the aircraft flutter (Q4928239) (← links)
- Bifurcation analysis of aero-engine's rotor system under constant maneuver load (Q5962985) (← links)
- Coupling dynamic behavior of aero-engine rotor system caused by rolling, pitching and yawing maneuver loads (Q6135667) (← links)
