Pages that link to "Item:Q623867"
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The following pages link to Analysis on the nonlinear response of cracked rotor in hover flight (Q623867):
Displaying 6 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)
- Nonlinear response analysis for a dual-rotor system with a breathing transverse crack in the hollow shaft (Q331209) (← links)
- Nonlinear response and dynamic stability of a cracked rotor (Q876089) (← links)
- Parametric instability of flexible rotor-bearing system under time-periodic base angular motions (Q2282917) (← links)
- Study on the chaotic dynamics in yaw-pitch-roll coupling of asymmetric rolling projectiles with nonlinear aerodynamics (Q2297036) (← links)