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