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

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

The compatibility between a composite beam cross-sectional analysis based on the variational asymptotic approach, and a helicopter rotor blade model which is part of a comprehensive rotorcraft analysis code is examined. It was found that the finite element cross-sectional analysis code VABS can be combined with a moderate deflection rotor blade model in spite of the differences between the form...

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ژورنال

عنوان ژورنال: International Journal of Solids and Structures

سال: 2009

ISSN: 0020-7683

DOI: 10.1016/j.ijsolstr.2008.09.017