TY - GEN
T1 - Exact solutions for the linear static response of anisotropic composite beams under arbitrary loading and boundary conditions
AU - Doeva, Olga
AU - Masjedi, Pedram Khaneh
AU - Weaver, Paul M.
N1 - Publisher Copyright:
© 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All Rights Reserved.
PY - 2021
Y1 - 2021
N2 - The exact analytical solutions for static response of fully coupled composite beams subject to arbitrary loading and boundary conditions are presented. The analysis is based on the Euler-Bernoulli and Timoshenko beam theories. The governing equations are presented as a set of coupled inhomogeneous ordinary differential equations, and then expressed in a compact matrix form, which enables applying the method of direct integration to derive the exact analytical solutions. The solutions are obtained for arbitrary concentrated and non-uniformly distributed loads while classical and elastically retrained boundary conditions are considered in the formulation. Several numerical examples are given and the results are compared to those obtained from the Chebyshev Collocation Method. Different length-to-thickness ratios are considered to highlight the importance of shear deformation in short beams. The proposed analytical solutions are suitable for benchmarking and convergence studies of numerical solutions.
AB - The exact analytical solutions for static response of fully coupled composite beams subject to arbitrary loading and boundary conditions are presented. The analysis is based on the Euler-Bernoulli and Timoshenko beam theories. The governing equations are presented as a set of coupled inhomogeneous ordinary differential equations, and then expressed in a compact matrix form, which enables applying the method of direct integration to derive the exact analytical solutions. The solutions are obtained for arbitrary concentrated and non-uniformly distributed loads while classical and elastically retrained boundary conditions are considered in the formulation. Several numerical examples are given and the results are compared to those obtained from the Chebyshev Collocation Method. Different length-to-thickness ratios are considered to highlight the importance of shear deformation in short beams. The proposed analytical solutions are suitable for benchmarking and convergence studies of numerical solutions.
UR - http://www.scopus.com/inward/record.url?scp=85100310441&partnerID=8YFLogxK
U2 - 10.2514/6.2021-1044
DO - 10.2514/6.2021-1044
M3 - Conference contribution
AN - SCOPUS:85100310441
SN - 9781624106095
T3 - AIAA Scitech 2021 Forum
SP - 1
EP - 19
BT - AIAA Scitech 2021 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021
Y2 - 11 January 2021 through 15 January 2021
ER -