Abstract
This paper deals with the modelling and dynamic analysis of thin or slender flexible bodies characterized by axial motion, contacts and friction interaction. Such mechanical systems can be found in cable applications, in petroleum drilling industry, in biomedical applications and in nuclear equipments. An original combination of the absolute nodal coordinate formulation and the classical finite element method is used for the modelling of flexible slender structures moving inside flexible tubes and channels considering the overall system vibration. In a nuclear power plant, it allows to analyse mainly the influence of guide thimbles vibration on the control rod drop. The novelty of the introduced methodology is also in the original usage of the absolute nodal coordinate formulation in the problems of nuclear engineering. All the interaction phenomena such as effect of fluid flow, contact forces, gravitation and buoyancy forces are considered in the mathematical model. The particular application of the presented methodology on the problem of the nuclear control rod drop through vibrating bowed guide thimble helps to formulate interesting conclusions on the rod drop time affected by vibrating guide thimbles.
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Data availability statement
The datasets generated during and analysed during the current study are available from the corresponding author on reasonable request.
Notes
VVER, also referred to as WWER, stands for water-cooled and water-moderated energetic reactor, number 1000 refers to the power provided by the reactor.
Abbreviations
- \(\alpha \) :
-
Rayleigh proportional damping parameter
- \(\alpha _c\) :
-
Angle defining the contact position
- \(\beta \) :
-
Rayleigh proportional damping parameter
- \(\delta \) :
-
Contact penetration depth
- \(\eta \) :
-
FE dimensionless parameter
- \(\kappa \) :
-
Curvature of element centre line
- \(\mathbf{B} \) :
-
Global damping matrix
- \(\mathbf{B} _{e}\) :
-
Element damping matrix
- \(\mathbf{e} \) :
-
Vector of ANCF nodal coordinates
- \(\mathbf{e} _\mathrm{FEM}\) :
-
Vector of FE beam nodal coordinates
- \(\mathbf{f} _\mathrm{cont}^\mathrm{(CR)}\) :
-
Global vector of contact forces for the CR
- \(\mathbf{f} _\mathrm{cont}^\mathrm{(GT)}\) :
-
Global vector of contact forces for the GT
- \(\mathbf{f} _\mathrm{drag}^\mathrm{(CR)}\) :
-
Global vector of drag forces for the CR
- \(\mathbf{f} _{e, \mathrm {cont}}^\mathrm{FEM}\) :
-
Generalized contact force vector of e-th FEM element
- \(\mathbf{F} _{e}^\mathrm{FEM}\) :
-
Contact forces vector in e-th FEM element
- \(\mathbf{f} _{k, \mathrm {cont}}^\mathrm{ANCF}\) :
-
Generalized contact force vector of k-th ANCF element
- \(\mathbf{f} _\mathrm{{kin}, { L}}^\mathrm{(GT)}\) :
-
Kinematical excitation of lower node
- \(\mathbf{f} _\mathrm{{kin}, { U}}^\mathrm{(GT)}\) :
-
Kinematical excitation of upper node
- \(\mathbf{F} _{p,k}^\mathrm{ANCF}\) :
-
Contact forces vector in p-th contact point of k-th ANCF element
- \(\mathbf{f} _\mathrm{st}^\mathrm{(CR)}\) :
-
Global vector of gravitation and buoyancy for the CR
- \(\mathbf{g} \) :
-
Gravitational acceleration vector
- \(\mathbf{G} _e\) :
-
Generalized gravity force vector
- \(\mathbf{I} \) :
-
Identity matrix
- \(\mathbf{K} _{ C}\) :
-
Global coupling stiffness matrix of spacer grids
- \(\mathbf{K} \) :
-
Global stiffness matrix
- \(\mathbf{K} _e^\mathrm{tang}\) :
-
ANCF tangent stiffness matrix
- \(\mathbf{M} \) :
-
Global mass matrix
- \(\mathbf{M} _e\) :
-
Element mass matrix
- \(\mathbf{N} \) :
-
Matrix of FEM shape functions
- \(\mathbf{Q} \) :
-
Global vector of elastic forces
- \(\mathbf{q} \) :
-
Global vector of nodal coordinates
- \(\mathbf{Q} _e\) :
-
Vector of element elastic forces
- \(\mathbf{q} _e\) :
-
Vector of arbitrary beam point displacements and rotation angles
- \(\mathbf{q} _s\) :
-
Vector of spacer grids deformations
- \(\mathbf{Q} _\mathrm{be}\) :
-
Vector of bending elastic forces
- \(\mathbf{Q} _\mathrm{le}\) :
-
Vector of longitudinal elastic forces
- \(\mathbf{r} \) :
-
Position vector of a beam point
- \(\mathbf{r} ^j\) :
-
Position vector of node j
- \(\mathbf{r} ^j_{,x}\) :
-
Gradient of position vector
- \(\mathbf{r} _c\) :
-
Position vector between cross-sectional centre points
- \(\mathbf{r} _c^\mathrm{CR}\) :
-
Global position vector of CR cross-sectional centre point
- \(\mathbf{r} _c^\mathrm{GT}\) :
-
Global position vector of GT cross-sectional centre point
- \(\mathbf{r} _D\) :
-
Position vector from GT centre to detected contact point
- \(\mathbf{S} \) :
-
Matrix of ANCF shape functions
- \(\omega _{b1}\) :
-
First bending eigenfrequency
- \(\omega _{b2}\) :
-
Second bending eigenfrequency
- \(\rho \) :
-
Material density
- \(\rho _c\) :
-
Water coolant density
- \(\rho _e\) :
-
Density of element e
- \(\rho _\mathrm{CR}\) :
-
Considered density of the CR
- \(\varepsilon _x\) :
-
Axial strain
- \(\varphi _x,\ \varphi _z\) :
-
Beam FE rotational angles
- \(\xi \) :
-
ANCF dimensionless parameter
- \(A^\mathrm{CR}\) :
-
Control rod cross-sectional area
- \(A_e\) :
-
Beam cross-sectional area
- \(c_f\) :
-
Friction coefficient
- \(C_v\) :
-
Drag coefficient
- D :
-
Damping ratio
- \(D_c\) :
-
Contact damping factor
- \(D_e\) :
-
Outer diameter of GT
- \(d_e\) :
-
Inner diameter of GT
- \(D_\mathrm{CR}\) :
-
Outer diameter of the CR
- \(D_{p, k}^e\) :
-
Detected contact point between k-th ANCF element and e-th FEM element
- E :
-
Young’s modulus
- e :
-
Index of FEM beam element
- \(E_e\) :
-
Young’s modulus of element e
- F :
-
Free FE beam nodes
- f :
-
Range of excitation frequencies
- \(F_b\) :
-
Buoyancy force
- \(F_N\) :
-
Normal contact force
- \(F_T\) :
-
Friction force
- \(F_\mathrm{drag}\) :
-
Hydrodynamic drag force
- g :
-
Index of spacer grid (\(g = 2i\) in FEM node i)
- \(g_\mathrm{const}\) :
-
Gravitational acceleration
- i :
-
Index of FEM beam node
- \(I_e\) :
-
Second moment of area
- j :
-
Index of ANCF beam node
- K :
-
Contact stiffness
- k :
-
Index of ANCF beam element
- \(k_{g,x},\ k_{g,z}\) :
-
Spacer grid stiffness
- L :
-
Lower FE beam node
- \(l_e\) :
-
Element length
- \(l_\mathrm{CR}\) :
-
Total length of the CR
- M :
-
Total number of ANCF nodes
- m :
-
Weight of body
- N :
-
Total number of FE beam nodes
- n :
-
Hertz contact exponent
- \(N_b\) :
-
FE shape functions, \(b = 1,\ \dots ,\ 8\)
- \(n_{C}\) :
-
Total number of contact points per element
- p :
-
Index of ANCF beam element contact point
- \(r_\mathrm{CR}\) :
-
CR radius
- \(r_\mathrm{GT}\) :
-
GT radius
- \(S_a\) :
-
ANCF shape functions, , \(a = 1,\ \dots ,\ 4\)
- \(t_\mathrm{lim}\) :
-
Drop time limit value
- U :
-
Upper FE beam node
- \(U_e\) :
-
Element deformation energy
- \(u_x,\ u_z\) :
-
Beam FE lateral displacements
- \(V_e\) :
-
Element volume
- \(v_r\) :
-
Velocity threshold value for friction
- \(v_Y\) :
-
Vertical velocity in the contact point
- \(v_\mathrm{CR}\) :
-
CR velocity
- \(v_\mathrm{flow}\) :
-
Fluid flow velocity
- x :
-
Local axial coordinate of ANCF element
- \(X,\ Y,\ Z\) :
-
Global coordinate system
- \(x_{C_p}\) :
-
Axial parameter of ANCF contact points
- \(x_{g,st}\) :
-
Lateral static deformation of LBS in SG
- \(x_\mathrm{max}\) :
-
GT maximum deformation
- \(y_\mathrm{{loc}, D}\) :
-
FE beam axial coordinate of detected contact point
- \(y_\mathrm{loc}\) :
-
local axial parameter of FE beam
- \(z_{g, \mathrm {st}}\) :
-
Lateral static deformation of LBS in SG
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Acknowledgements
The work was supported from European Regional Development Fund-Project “Research and Development of Intelligent Components of Advanced Technologies for the Pilsen Metropolitan Area (InteCom)” (No. CZ. 02.1.01/0.0/0.0/17_048/0007267) and by the Motivation system of the University of West Bohemia—Part Postdoc.
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Bulín, R., Dyk, Š. & Hajžman, M. Nonlinear dynamics of flexible slender structures moving in a limited space with application in nuclear reactors. Nonlinear Dyn 104, 3561–3579 (2021). https://doi.org/10.1007/s11071-021-06582-1
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DOI: https://doi.org/10.1007/s11071-021-06582-1