Acta Mechanica

, Volume 216, Issue 1–4, pp 207–223 | Cite as

Dynamic stability of linear parametrically excited twisted Timoshenko beams under periodic axial loads

Article

Abstract

In this paper, the parametric instability of twisted Timoshenko beams with various end conditions and under an axial pulsating force is studied. The equations of motion in the twisted frame are derived using a finite element method. Based on Bolotin’s method, a set of second-order ordinary differential equations with periodic coefficients of Mathieu–Hill type is formed to determine the instability regions for twisted Timoshenko beams. A dynamic instability index is defined and used as an instability measure to study the influence of various parameters. The effects of beam length, inertia ratio, pre-twist angle, dynamic component of axial force and restraint condition on the instability regions and dynamic instability index of the twisted beam are investigated and discussed.

Keywords

Dynamic Stability Timoshenko Beam Instability Region Timoshenko Beam Theory Bernoulli Beam Theory 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

List of symbols

A

Cross-sectional area

b

Width of the beam

DII

Dynamic instability index

d

Displacement matrix in frame ξηZ

d(e)

Displacement function of the beam

E

Young’s modulus

Fz(t)

Time-dependent axial load

F

Global stiffness matrix due to unit axial force

F(e)

Element stiffness matrix due to unit axial force

G

Shear modulus

IXX, IYY, IXY

Area moments and product of inertia in frame XYZ

Iξ, Iη

Principal area moments of inertia in frame ξηZ

JXX, JYY, JXY

Mass moments and product of inertia per unit length in frame XYZ

Jξ, Jη

Principal mass moments of inertia per unit length in frame ξηZ

K

Global stiffness matrix

\({\overline{\bf{K}}_1, \overline{\bf{K}}_2, \overline{\bf{K}}_3, \overline{\bf{K}}_4}\)

Stiffness coefficient matrices due to the bending and shear effects

KB

Global stiffness matrix due to the bending and shear effects

\({{\boldsymbol K}_B^{(e)}}\)

Element stiffness matrix due to the bending and shear effects

\({{\boldsymbol K}_F^{(e)}}\)

Element stiffness matrix due to axial force

L

Beam length

Le

Beam element length

Lref

Reference beam length

m

beam mass per unit length

M

Global inertia matrix

M(e)

Element inertia matrix

\({\overline{\bf{M}}}\)

Inertia coefficient matrix

N

Transformation matrix between displacement function and nodal displacements

N1, N2

Shape functions of linear beam element

Pcr

Critical static buckling load

\({\overline{{P}}_{\rm cr}}\)

Dimensionless critical buckling load

p

Global displacement matrix

p(e)

Element displacement matrix

q

Constant vector

R

Inertia ratio of beam cross-section

T

Kinetic energy

t

Thickness of the beam

uX, uY

Total transverse displacements in frame XYZ

uξ, uη

Transverse displacements in frame ξηZ

uξ1, uη1, uξ 2, uη2

Nodal transverse displacements in frame ξηZ

V

Potential energy

W

Work produced by the axial load

Z

Axial coordinate

κ

Shear correction factor

ρ

Density of the beam

ω

Natural frequency

Ω

Disturbing or boundary frequency

\({\overline{{\Omega}}}\)

Boundary frequency ratio

Δ Ω

Opening of instability region

α

Static load factor

β

Dynamic load factor

βo

Twist angle per unit length

\({\phi}\)

Total twist angle

\({\varphi_{x}, \varphi_{y}}\)

Angles of rotation in frame XYZ

\({\varphi_{\xi}, \varphi_{\eta}}\)

Angles of rotation in frame ξηZ

\({\varphi_{\xi 1}, \varphi_{\eta 1}, \varphi_{\xi 2}, \varphi_{\eta 2}}\)

Nodal angles of rotation in frame ξηZ

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Copyright information

© Springer-Verlag 2010

Authors and Affiliations

  1. 1.Department of Mechanical EngineeringChinese Culture UniversityTaipeiTaiwan, ROC

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