Pages that link to "Item:Q3495835"
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The following pages link to Vibration analysis of composite turbopropellers using a nonlinear beam-type finite-element approach (Q3495835):
Displaying 8 items.
- Aeroelastic tailoring analysis for advanced turbo propellers with composite blades (Q1198343) (← links)
- Vibration and flutter of stiff-inplane elastically tailored composite rotor blades (Q1324699) (← links)
- A comprehensive finite element model for tapered composite wing structures (Q3112959) (← links)
- (Q3760067) (← links)
- Finite-Element-Based Nonlinear Modal Reduction of a Rotating Beam with Large-Amplitude Motion (Q4817931) (← links)
- Period Doubling Motions of a Nonlinear Rotating Beam at 1:1 Resonance (Q5498611) (← links)
- Accurate reduced-order models for a simple rotor blade model using nonlinear normal modes. (Q5952777) (← links)
- Asymptotic analysis of Timoshenko-like orthotropic beam with elliptical cross-section (Q6049502) (← links)