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

  • Published:2009-05 Issue:10 Volume:46 Page:2186-2200
  • ISSN:0020-7683
  • Container-title:International Journal of Solids and Structures
  • language:en
  • Short-container-title:International Journal of Solids and Structures

Author:

Friedmann Peretz P.,Glaz Bryan,Palacios Rafael

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science,Modelling and Simulation

Reference38 articles.

1. Theory of anisotropic thin-walled closed-cross-section beams;Berdichevsky;Composites Engineering,1992

2. A large displacement formulation for anisotropic beam analysis;Bori;Meccanica,1986

3. A beam finite element non-linear theory with finite rotation;Cardona;International Journal for Numerical Methods in Engineering,1988

4. VABS: a new concept for composite rotor blade cross-sectional modeling;Cesnik;Journal of the American Helicopter Society,1997

5. A consistent co-rotational formulation for non-linear, three-dimensional beam-elements;Crisfield;Computer Methods in Applied Mechanics and Engineering,1990
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