Pages that link to "Item:Q2009963"
From MaRDI portal
The following pages link to Flutter analysis of bending-torsion coupling of aero-engine compressor blade with assembled clearance (Q2009963):
Displaying 8 items.
- The sliding mode control for an airfoil system driven by harmonic and colored Gaussian noise excitations (Q2307005) (← links)
- Investigation of the nonlinearity effect of the shrouded blade assemblies on their forced vibrations (Q2679148) (← links)
- (Q2787270) (← links)
- Bifurcation of resonance during flutter of the blades of a turbocompressor rotor (Q2836569) (← links)
- Flutter with limit cycle of oscillations of turbocompressor rotor blades (Q2838921) (← links)
- Prediction of transient engine loads and damage due to hollow fan blade-off (Q3426686) (← links)
- Transient Response of High Dimensional Nonlinear Dynamic System for a Rotating Cantilever Twisted Plate (Q5157005) (← links)
- Early warning of noise-induced catastrophic high-amplitude oscillations in an airfoil model (Q6560594) (← links)
