A General-Purpose Implementation of the Mixed Formulation of the Geometrical Exact Beam Theory

GEBT (Geometrically Exact Beam Theory), a general-purpose tool for nonlinear analysis of composite beams, is developed to meet the design challenges associated with future air vehicles featuring highly-∞exible slender components. GEBT is based on the mixed formulation of the geometric exact beam theory which can capture all geometric nonlinearities due to large de∞ections and rotations, subject to the strains being small. Coupled with VABS, a general-purpose cross-sectional analysis, GEBT can efiectively analyze geometric nonlinear behavior of slender structures having arbitrary cross-sections made of arbitrary materials. In comparison to the original, nonlinear, three-dimensional analysis, the computational cost is signiflcantly reduced without noticeable loss of accuracy.

[1]  Maxwell Blair,et al.  A Design Optimization Strategy for Micro Air Vehicles , 2007 .

[2]  Dewey H. Hodges,et al.  Generalized Timoshenko Theory of the Variational Asymptotic Beam Sectional Analysis , 2005 .

[3]  Dewey H. Hodges,et al.  Flight Dynamics of Highly Flexible Aircraft , 2008 .

[4]  D. Hodges,et al.  Fundamentals of Structural Stability , 2006 .

[5]  O. Bauchau Computational Schemes for Flexible, Nonlinear Multi-Body Systems , 1998 .

[6]  V. Berdichevskiĭ Variational-asymptotic method of constructing a theory of shells , 1979 .

[7]  Robert A. Canfield,et al.  Structural Optimization of Joined-Wing Beam Model with Bend/Twist Coupling Using ESL , 2009 .

[8]  Carlos E. S. Cesnik,et al.  Limit-cycle oscillations in high-aspect-ratio wings , 2002 .

[9]  Carlos E. S. Cesnik,et al.  Finite element solution of nonlinear intrinsic equations for curved composite beams , 1995 .

[10]  Nicholas S. Green,et al.  Structural Optimization of Joined-Wing Beam Model with Bend-Twist Coupling Using Equivalent Static Loads , 2012 .

[11]  Wenbin Yu,et al.  Variational asymptotic modeling of composite dimensionally reducible structures , 2002 .

[12]  Carlos E. S. Cesnik,et al.  On Timoshenko-like modeling of initially curved and twisted composite beams , 2002 .

[13]  Robert A. Canfield,et al.  Joined-Wing Aeroelastic Design with Geometric Nonlinearity , 2005 .

[14]  Maxwell Blair,et al.  AVEC: A Computational Design Framework for Conceptual Innovations , 2006 .

[15]  D. Hodges A mixed variational formulation based on exact intrinsic equations for dynamics of moving beams , 1990 .

[16]  Dewey H. Hodges,et al.  Nonlinear Composite Beam Theory , 2006 .

[17]  Dewey H. Hodges,et al.  Nonlinear Beam Kinematics by Decomposition of the Rotation Tensor , 1987 .