10.01.2013 Views

Design Report Guided Missile Submarine SSG(X) - AOE - Virginia ...

Design Report Guided Missile Submarine SSG(X) - AOE - Virginia ...

Design Report Guided Missile Submarine SSG(X) - AOE - Virginia ...

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

<strong>SSG</strong>(X) <strong>Design</strong> – VT Team 3 Page 72<br />

For the optimization, initial estimates were made for the Expanded Area Ratio (EAR), Pitch to Diameter Ratio<br />

and propeller diameter (DP). Using the Wageningen B Series, POP optimizes all these values. The wake fraction is<br />

updated using the optimized DP. The optimization is redone with the new wake fraction. This iteration process is<br />

performed until DP does not change. During the optimization process, 7-bladed propellers were found to be the most<br />

efficient.<br />

The optimization results were used to evaluate the snorkel and sprint conditions to ensure the efficiencies<br />

satisfied the ORD and that the propeller does not cavitate. The POP program uses Burrill’s Simple Cavitation<br />

Diagram, shown in Figure 65; this is a plot of the mean thrust loading against the local cavitation number. To keep<br />

the signatures as small as possible, a strict 5% Burrill back cavitation criteria is used. If the propeller violates the<br />

cavitation criteria, the POP program gives a warning and changes must be made. The most effective change is a<br />

decrease of P/D.<br />

Figure 65 - Burrill's Simple Cavitation Diagram [Principles of Naval Architecture]<br />

The iteration process is repeated until all ORD efficiencies are satisfied and the propeller does not cavitate<br />

during snorkel and sprint. The snorkel resistance calculation included a wave induced drag while snorkeling, which<br />

the original model did not include. Because of this the snorkel endurance did not satisfy the ORD requirement. To<br />

meet this requirement, 40 ltons of diesel fuel were added to the baseline design. Figure 66 and Figure 67 show the<br />

propeller curves for AIP endurance and AIP sprint respectively. Figure 68 shows the propeller curves for snorkel<br />

endurance.<br />

Figure 66 - Propeller Curves for AIP Endurance (5 knt)

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!