TY - JOUR
T1 - Nonconservative Stability Analysis of Columns with Various Loads and Boundary Conditions
AU - Fazelzadeh, S. Ahmad
AU - Tashakorian, Mohammad
AU - Ghavanloo, Esmaeal
AU - Friswell, Michael I.
AU - Amoozgar, Mohammadreza
PY - 2019/10/1
Y1 - 2019/10/1
N2 - In this paper, the stability analysis of the elastic columns subjected to seven different types of the nonconservative force is investigated on the basis of fully intrinsic beam equations. The generalized differential quadrature method is used for the discretization of the first-order intrinsic equations and corresponding boundary conditions. Altogether, four important boundary conditions—simply supported, clamped-simply supported, clamped-free, and clamped-clamped conditions—are considered. Furthermore, the effect of the combined action of an end-concentrated force and a distributed tangential follower force is investigated. To confirm the validity of the proposed intrinsic formulations, the present results are compared with those obtained from classical formulations. Our results reveal that the fully intrinsic formulation is a suitable framework to model nonconservative problems.
AB - In this paper, the stability analysis of the elastic columns subjected to seven different types of the nonconservative force is investigated on the basis of fully intrinsic beam equations. The generalized differential quadrature method is used for the discretization of the first-order intrinsic equations and corresponding boundary conditions. Altogether, four important boundary conditions—simply supported, clamped-simply supported, clamped-free, and clamped-clamped conditions—are considered. Furthermore, the effect of the combined action of an end-concentrated force and a distributed tangential follower force is investigated. To confirm the validity of the proposed intrinsic formulations, the present results are compared with those obtained from classical formulations. Our results reveal that the fully intrinsic formulation is a suitable framework to model nonconservative problems.
KW - Aeroelasticity
KW - Flexible wings
KW - Flexible aircraft
UR - https://www.scopus.com/record/display.uri?eid=2-s2.0-85078526447&origin=inward&txGid=2c419d18ae0c527e26e9a6e9109635cf
U2 - 10.2514/1.j057501
DO - 10.2514/1.j057501
M3 - Article
VL - 57
SP - 4269
EP - 4277
JO - AIAA Journal
JF - AIAA Journal
SN - 0001-1452
IS - 10
ER -