SHEAR7
With over ten years of industry use and continuous development, SHEAR7
is one of the leading modeling tools for the prediction of
vortex-induced vibration (VIV). The program’s forte is the VIV response
prediction of offshore structures subjected to spatially varying
currents; realistic of ocean environments. The program enables users to
estimate structural responses, mean drag force amplification factors and
predict fatigue damage. It is simple and fast to run with all the
results summarized in a convenient standard output file. The new release
allows for more accurate modeling of Strakes.
The nuts and bolts...
SHEAR7 is a mode superposition program, which evaluates which modes are
likely to be excited by vortex shedding and estimates the steady state,
cross-flow, VIV response in uniform or sheared flows. It is capable of
evaluating multi-mode, non-lock-in response, as well as single mode
lock-in response.
The program evaluates natural frequencies and mode shapes of cables and
beams with linearly varying or slowly varying tension and with a
variety of boundary conditions, including cantilevers and free hanging
risers. The program is capable of evaluating the natural frequencies and
mode shapes and VIV response of horizontal catenary cables and uses an
approximate structural model for inclined catenary cables.
The user may choose to compute natural frequencies and mode shapes in a separate program,
such as a finite element program and provide them as input to SHEAR7 in a
common.mds file. In this way, structures which are not in the standard
solution set of SHEAR7 may be evaluated.
SHEAR7 can be used to predict the cross flow RMS displacement and
stress; as well as fatigue damage rate and local drag amplification
coefficients.
Cylinders are not required to be of constant cross-section. The user
may also model sections of risers with VIV suppression devices (strakes
and fairings) as well as staggered buoyancy modules.
The basic solution technique used is modal analysis and iteration (to
account for the non-linear relationship between response and lift
coefficient.) The physical assumption is that the power input (by lift
force) and power output (through damping) for each mode should be in
balance in a steady state. From initial values of lift and damping
coefficients, the program finds the lift and damping coefficients in a
balanced state through iteration. The converged lift and damping
coefficients are used to compute cylinder response.
Throughout the years of development, SHEAR7 has remained a very
simple to use program, that can quickly be run from a standard desktop
computer. Once the program has run, an out file is produced which
conveniently summarizes the results.
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Incorporate your own lift coefficient and damping data from experiments to predict behavour of long flexible structures.
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The ability to define the lift and damping behaviour separately for each zone on the structure.
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Results can be produced in the time domain for rainflow fatigue calculations or incorporation with other modeling programs.
Previous Release: Version 4.5
SHEAR7 version 4.5 was the twelfth
distribution of SHEAR7. The use of the program is similar to that of
versions 4.0-4.4 but the way in which the program works has been changed
considerably. This reflects the findings of recent research, in
particular that of the MIT/DEEPSTAR program involving towing slender
pipes in the Gulf Stream offshore Miami. The most significant
modification introduced in version 4.5 involves a change in the way
power-in regions are apportioned in time and space.
In V4.4 and in all earlier versions of the program
utilized a ‘competing modes’ model of Vortex Induced Vibrations (VIV),
whereas all potentially responding modes competed among each other for
power-in length on the riser. Whenever response in more than one mode
was feasible, the whole power-in region was subdivided into individual
power-in regions, one per mode. Any overlaps between modal power-in
regions were removed. The greater the number of modes left above the
cutoff power level, the smaller the individual power-in regions
became. This had the effect of reducing the response of each mode.
Recent research has shown that this in not seen on typical risers.
Rather, each mode appears one at a time. Over a long period several
modes may come and go, sharing the time that VIV is experienced. Each
mode has a much larger power-in region than would be permitted by
removing spatial overlap in power-in regions. Each mode has more
power-in and responds with larger amplitude than would be predicted in
the old method of response computation.
Time Sharing Concept
SHEAR7 versions 4.5 and 4.6 utilize the concept of
time-sharing between the modes, making spatial overlap elimination
between the modes unnecessary. The concept of time sharing is based on
observations from the Gulf Stream, Deepstar-funded, slender pipe
experiments. The data revealed that VIV response is dominated by one
single frequency at a time, with the response switching frequently
among frequencies.
The time sharing principle is illustrated for a low
mode number example below. Similar to the way that previous program
versions operated, the program first performs an initial modal power
calculation using full bandwidth for the power-in region to form a basis
for deciding relative modal dominance in the final modal calculation.
In versions 4.5 and 4.6, after the initial power calculation, modes
are allowed to respond with the full input bandwidth (power-in region)
but the time over which they are allowed to respond is reduced in
accordance with calculated time sharing probabilities. As the default,
the time sharing probabilities are proportional to power ratios.

The program still works in the frequency domain and it still uses the Modal Superposition Method.
Version 4.6
SHEAR7 version 4.6 introduced enhancements to
version 4.5, while utilizing the same time sharing concept. In
particular, V4.6 allowed a vastly improved modeling of strakes, both
partial and close to full coverage.
The program enhancements included:
- Adding the option to model hydrodynamic forces on
strakes in terms of sectional damping as an alternative to
predominantly negative fluctuating lift coefficient (lift curve);
- Introduction of material properties varying along
the model (multiple sets of moduli of elasticity and S-N Curves
supported); those are defined individually in each sectional zone;
- The numbers of the S-N Curves that can be defined or/and used in a single *.dat file are unlimited.
- The maximum allowable number of S-N curve
segments is increased to 10 (from 5 that was supported in older
versions); 1 to 10 segments can be used in order to define each of the
multiple S-N Curves.
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