Pages that link to "Item:Q5952778"
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The following pages link to Assessment of beam modeling methods for rotor blade applications. (Q5952778):
Displaying 10 items.
- Maximum stiffness and minimum weight optimization of laminated composite beams using continuous fiber angles (Q381589) (← links)
- Free vibration and dynamic stability of rotating thin-walled composite beams (Q388283) (← links)
- Equations of motion of rotating composite beam with a nonconstant rotation speed and an arbitrary preset angle (Q475497) (← links)
- A moderate deflection composite helicopter rotor blade model with an improved cross-sectional analysis (Q545099) (← links)
- Linear viscoelastic analysis of straight and curved thin-walled laminated composite beams (Q837335) (← links)
- An asymptotic analysis of composite beams with kinematically corrected end effects (Q957392) (← links)
- A Rankine-Timonshenko-Vlasov beam theory for anisotropic beams via an asymptotic strain energy transformation (Q1668333) (← links)
- Isogeometric analysis of composite beams with arbitrary cross-section using dimensional reduction method (Q2309778) (← links)
- Accurate reduced-order models for a simple rotor blade model using nonlinear normal modes. (Q5952777) (← links)
- A three-unknown refined shear beam model for the bending of randomly oriented FG-CNT/fiber-reinforced composite laminated beams rested on a new variable elastic foundation (Q6051284) (← links)
