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Trans RINA, Vol 154, Part C1, Intl J Marine Design, Jan - Jun 2012 irrespective of vessel length). The scatter is due to


changes in the other design parameters, with the variation about the mean giving some indication of the scope for possible optimisation of these parameters. The greater the scatter, the more influence the other parameters have on the performance.


4. PRACTICAL APPLICATION OF DESIGN- SPACE EXPLORATION RESULTS


Several typical scenarios where the design-space


knowledge, captured in the response surfaces, can help the design team have been identified. These are discussed in more detail below.


4.1 ISO-PARAMETRIC VARIATION


Iso-parametric lines and surfaces are useful for answering questions such as: “How is the required delivered power affected if I change the vessel length whilst keeping the other parameters constant?”. Because there is an infinite number of combinations of values of the design parameters that are kept fixed, it is normal to choose some sensible baseline design from which to make the single (or twin) parameter variations.


The sensitivity of performance measures to certain design parameters can be gauged by looking at the shape of the iso-parametric surfaces. For instance, for the example application, it can be seen in Figure 7, that the required delivered power is much more sensitive to length than it is to beam. Thus there is less of a trade-off in power if the beam needs to be changed (to improve another aspect, for instance) than to change the vessel length.


simple interpolation is required to obtain the performance measures (instead of direct analysis with computationally intensive simulation tools). Some typical optimisation scenarios are described below.


4.2 (a) Design Genesis


When performing an initial search for viable design candidates which will be possible solutions to the design brief, all design parameters are allowed to vary within the range covered in the design-space. Since multiple performance measures have been calculated, a multi- objective optimisation may be appropriate, leading to a Pareto-front


of optimum design alternatives with


different compromises between each of the performance objectives. By examining the Pareto-front solutions, a feel can be gained for the trade-offs that might be required to improve a preferred performance measure. This can help the designer answer questions such as “What will happen to the stability and sea-keeping comfort if I would like to reduce the vessel resistance?”


Within the FFW, it is straightforward to perform separate optimisations for each of the individual performance measures, starting from the same baseline vessel. Figure 8 shows how the design parameters differ when the vessel is optimised for the different performance measures. Five vessels are shown, the baseline vessel and then a vessel optimised for each of the individual performance measures of interest. The points of the star are the normalised values of each of the design parameters. It can be seen that the vessel optimised for stability is quite different


from the other vessels: a


shorter, beamier vessel with high midship area is favoured. (Referring back to Figure 6, it can be seen from the initial design-space investigation, that shorter vessels


generally have better stability than longer


vessels.) The vessels optimised for resistance and sea- keeping are longer and narrower (as might be expected). These results can be used to answer questions such as: “How does the design for minimum resistance compare to that which offers best comfort in a seaway?”.


Figure 7: Response surface for Power vs. Length and Beam.


4.2 OPTIMISATION


Automated optimisation has been well documented over recent years (see COMPIT conferences for example: www.compit.info). The data obtained from the design- space exploration and captured in the response surfaces is ideally suited to such optimisation, because only a


Figure 8: Normalised Optimum Design Parameter Values for Different Performance Measures.


©2012: The Royal Institution of Naval Architects


C-23


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