Aeroelastic stability of composite hingeless rotors with advanced configurations

This publication has 9 references indexed in Scilit:

• Finite element solution of nonlinear intrinsic equations for curved composite beams
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1995
• Aeroelastic stability of composite rotor blades in hover
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1995
• Coupling of a State-Space Inflow to Nonlinear Blade Equations and Extraction of Generalized Aerodynamic Force Mode Shapes
  Applied Mechanics Reviews, 1993
• Variational-Asymptotical Analysis of Initially Curved and Twisted Composite Beams
  Applied Mechanics Reviews, 1993
• Aeroelastic stability of composite hingeless rotor blades in hover—Part I: Theory
  Mathematical and Computer Modelling, 1993
• A Multibody Formulation for Helicopter Structural Dynamic Analysis
  Journal of the American Helicopter Society, 1993
• On a simplified strain energy function for geometrically nonlinear behaviour of anisotropic beams
  Composites Engineering, 1992
• Unified nonlinear analysis for nonhomogeneous anisotropic beams withclosed cross sections
  AIAA Journal, 1991
• A mixed variational formulation based on exact intrinsic equations for dynamics of moving beams
  International Journal of Solids and Structures, 1990