Pages that link to "Item:Q2296858"
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The following pages link to Research on vibration performance of the nonlinear combined support-flexible rotor system (Q2296858):
Displaying 8 items.
- Nonlinear vibration phenomenon of an aircraft rub-impact rotor system due to hovering flight (Q314316) (← links)
- Vibrations of a single-disk rotor on nonlinear supports (Q353492) (← links)
- Combined resonance of low pressure cylinder-generator rotor system with bending-torsion coupling (Q414200) (← links)
- Nonlinear vibration analysis of a rotor system using component mode synthesis method (Q1420078) (← links)
- Nonlinear and linear phenomenon investigation of coupled vibration of a multi-disc rotor based on multi-mistuned blades length or multi-disordered staggle angle blades (Q2089145) (← links)
- Vibration characteristic analysis of flexible rotor-bearing system subjected to external combined loads (Q2168410) (← links)
- Computational-experimental evaluation of stiffness response in elastic supports of rotor systems (Q2679178) (← links)
- Nonlinear forced vibration analysis of spinning shaft‐disk assemblies under sliding bearing supports (Q5159606) (← links)
