FREE VIBRATION ANALYSIS OF TRIPLY COUPLED PRE-TWISTED ROTOR BLADES BY THE DIFFERENTIAL QUADRATURE METHOD
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Publication:2846055
DOI10.1142/S0219455411004014zbMath1271.74183MaRDI QIDQ2846055
M. R. Forouzan, O. Sepahi, P. Malekzadeh
Publication date: 5 September 2013
Published in: International Journal of Structural Stability and Dynamics (Search for Journal in Brave)
differential quadrature methodfree vibrationdynamic characteristicspre-twisted rotor bladetriple coupling
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Cites Work
- FREQUENCIES OF A CIRCULAR PLATE WEAKENED ALONG AN INTERNAL CONCENTRIC CIRCLE
- NUMERICAL SOLUTIONS TO THE FREE VIBRATION PROBLEM OF MINDLIN SECTOR PLATES USING THE DISCRETE SINGULAR CONVOLUTION METHOD
- DYNAMIC STIFFNESS MATRIX FOR FLEXURAL-TORSIONAL, LATERAL BUCKLING AND FREE VIBRATION ANALYSES OF MONO-SYMMETRIC THIN-WALLED COMPOSITE BEAMS
- An efficient differential quadrature methodology for free vibration analysis of arbitrary straight-sided quadrilateral thin plates
- Dynamics of helicopter rotor blades
- Vibration Modes of Centrifugally Stiffened Beams
- Dynamic characteristics of rotor blades
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