A moderate deflection composite helicopter rotor blade model with an improved cross-sectional analysis

DOI10.1016/j.ijsolstr.2008.09.017zbMath1215.74042OpenAlexW2138155498MaRDI QIDQ545099

Rafael Palacios, Bryan Glaz, Peretz P. Friedmann

Publication date: 22 June 2011

Published in: International Journal of Solids and Structures (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.ijsolstr.2008.09.017

zbMATH Keywords

composite beamshelicopter rotor bladesVABS

Mathematics Subject Classification ID

Rods (beams, columns, shafts, arches, rings, etc.) (74K10) Composite and mixture properties (74E30)

Cites Work

• Asymptotic treatment of the trapeze effect in finite element cross-sectional analysis of composite beams
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• A beam finite element non-linear theory with finite rotations
• Nonlinear Beam Kinematics by Decomposition of the Rotation Tensor
• Non‐linear dynamics of three‐dimensional rods: Exact energy and momentum conserving algorithms
• Computational aspects of vector‐like parametrization of three‐dimensional finite rotations
• Assessment of beam modeling methods for rotor blade applications.