Huang 1993
Huang 1993
Huang 1993
Technical Note
A numerical approach for predicting the snap loading of marine cables operating
in alternating taut-slack conditions is presented. The modelling is based upon the
lumped-mass-and-spring method with modifications to take into account the bi-
linear axial stiffnessof the cable. The resulting governing equations are integrated
in the time domain using the modified Euler method. Numerical examples are
given and comparisons of the numerical results and the experimental results
available are made which demonstrate the validity of the present method.
Z
solutions of second-order systems in the time domain,
the Newmark family of methods is perhaps most widely
used for its accuracy and stability. For the highly
nonlinear marine cable dynamics, however, the appli-
cation of the Newmark's methods is not convenient as
additional computational effort is needed for iteration.
The application is further complicated by the response-
dependent nature of the forces such as tension and fluid
drag, especially for cables operating in taut-slack Fig. 1. Coordinate system and discretisation
conditions. In comparison, the modified Euler method
is considerably simpler than the Newmark's methods. massless elastic segments. All forces along the cable are
The explicit nature of the scheme makes it easily assumed to be concentrated at the mass points which are
adaptable to nonlinear dynamic analysis. numbered by i running from 0 at one end to N at the
other. By invoking Newton's law of motion for the i-th
node on the line, we have the following equation of
motion in the Cartesian coordinate system:
1
2 MATHEMATICAL MODELLING
400
280
z~ 240
bl
t- 180
HAXZHUH
120
B - m
/ _, -
80
NZNINIJI4 ~-4~--~'--1~--"---~
4O
0 I I I I I I I
-.I .t .3 .5 .7 .9 1.1 t.3 .5
FREGUENCY (Hz)
Fig. 2. Comparison between the numerical and experimental results (excitation amplitude 0.025 m)
A numerical method for predicting snap loading of marine cables 237
400
280
240
200
i- t00
NAXINUN
t20
m []
m
80
NZNZNUN
40
0 I I I I I I I
t .1 .3 .5 .7 .9 t.t 1.3 t.5
FREQUENCY (Hz)
Fig. 3. Comparison between the numerical and experimental results (excitation amplitude 0.05 m)
set to zero. The hydrodynamic drag on the i-th node is known motions is considered. In this case,
expressed as one-half of the drag acting on each of the
two segments on either side of that node. The drag on Xo(t) = 0
each segment is resolved into two components, namely, yo( t) = 0 (2)
the normal and tangential, each a function of the
relative velocity in that direction. Zo( t) = 0
and
2.2 Boundary and initial conditions XN(t ) : XtN
280
240
8O m -- II
NZNZHUN
4O
0 I I ! I I I I
--.t .1 .~ .5 ,7 .9 1,4 1.3 .5
w Y (~)
Fig. 4. Comparison between the numerical and experimental results (excitation amplitude 0"075m)
238 S. Huang, D. Vassalos
m
400
EXPERINENT (FYLLIN6 & WOLD 19791
380 " PRESENT NETHOD
320
280
240
2OO
uJ
p-
t60
t20 B
80
40
0 I I I I I IIr''nk I
- I .I .3 .5 .7 .9 1.1 '1.3 4.5
FREGUENCY (Hz)
Fig. 5. Comparison between the numerical and experimental results (excitation amplitude 0-1 m)
conditions must be specified for each node on the line. At must be sufficiently small to describe the response. A
This includes both the initial positions and initial recommended value for At is one eightieth of the small
velocities, as required by the second order ordinary period in the discretised cable system.
differential equations.
4 R E S U L T S AND D I S C U S S I O N
3 NUMERICAL INTEGRATION Model tests on cable snap tension were performed in the
Ship Research Institute of Norway 8 which consisted of
For the numerical integration of the mixed initial- restraining one end of a horizontally placed sagged cable
boundary-value problem defined by Eq. (1) and its and exciting the other end sinusoidally in the horizontal
associated boundary and initial conditions, the modified direction with known amplitude and frequency. The test
Euler method is used here. The numerical scheme can be results are used here to verify the validity and accuracy
expressed as follows:
ii
J~i
zi n
= A21 A22
LA31 "/132 A33Jn
A23[
~i n
(4) diameter:
length:
span:
Young's modulus:
0"01m
10.9774m
10.792 m
l0 ll N/m 2
Yi At (5) mass distribution: 0-61kg/m
Yi = Yi d-
range of amplitude: 0.025 m to 0"1 m
[xiI [xi]
-7i n + l -7i n range of frequency: 0 Hz to 1"2 Hz
Figures 2 to 5 show the maximum and minimum
Yi = Yi + Yi At (6) values of tension in the cable under excitations of
different amplitudes and frequencies for both the
Zi n+l Zi n Zi n+l numerical results and the experimental results. The
where At is the time step, and subscripts n and n + 1 agreement is good. It is. easy to see that when the
indicate their operant taking its value at time t = n A t or excitations are not severe, i.e., the excitation frequency is
t = (n + 1)At respectively. The procedure defined by low or the amplitude is small or both, the maximum and
equations (4)-(6) is carried out for all the nodes where minimum tensions are symmetrical with a constant
new displacements, velocities and accelerations are to be mean value which is equal to the static tension. When
evaluated. the excitation becomes severe, however, this symmetry
As the scheme is conditionally stable, At must be can no longer hold. As the minimum tension approaches
selected to satisfy the stability condition. 4 In addition, zero, that is the cable starts to operate in alternating
A numerical method for predicting snap loading of marine cables 239
-.4
-.6
-.8
-t .0
- t .2 I I I I
240 242 244 246 248 2110
TZHE (SECONDS}
(a)
&
-t
-2 | I | I
240 242 244 248 248 250
TZI~ (SECONDS)
(b)
t0
i -2
-4
"6
-8
-10 I I I I
240 242 244 248 248 26O
TZ~ (s[co~sl
(e)
Fig. 6. Time record of the vertical responses of the mid-point of the cable. (a) Displacement; (b) velocity; (c) acceleration.
(Excitation amplitude 0.05 m, frequency 0-75 Hz.)
240 S. Huang, D. Vassalos
-.4
-.8
-.8
-t .0
-1.2 | | I I
190 t92 t94 t98 tM 200
TZNE (SECONDS)
(a)
3.0
2.5
2.0
1.5
t.0
.5
0.0
-.5
-1.0 ! l I I
190 tg2 194 t96 t98 200
TI~ (SECONO)
(b)
20
15
,y // /
t0
5
iI i
i
/
0
#
n
/ /
n
-5 ! /
-t0
/ /
-t5
-20 i i I I
190 111~ 104 tM 4M
TZPlE ( ~ )
Fig. 7. Time record of the vertical responses of the mid-point of the cable. (a) Displacement; (b) velocity; (c) acceleration.
(Excitation amplitude 0.075 m, frequency I Hz.)
A numerical method for predicting snap loading of marine cables 241
-.4
-.O
1
X
-.8
- I .0
I I I I
-1.2t90
t92 194 196 t98 2OO
TZNE (SL=COmS)
Ca)
3.0
2.5
2.0
1.5
1.0
0.0
- t .0
190 192 194 196 t96 200
TTHE (SECOND)
(b)
i -:~
jjj
ij l ljl
-t5
-25
-30 I I I I
t92 ~94 t96 198 200
TIlE (SI~C0ND)
{c)
Fig. 8. Time record of the vertical responses of the mid-point of the cable. (a) Displacement; (b) velocity; (c) acceleration.
(Excitation amplitude 0.1 m, frequency 1 Hz.)
242 S. Huang, D. Vassalos