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A Rapid Development Process for Mar
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Table of Contents Abstract ... Ackn
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List ofTables Table I: Required Inp
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Figure 46: Surface Dynamic Pressure
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a long time to analyze, draw, fabri
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Simulation work is now commonly don
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Early theoretical analysis applied
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------------------------- provides
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As can be secn in Table I, the lift
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propeller geometry has to be entere
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avoid cavitation; however, it decre
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l" ........... ,... __ .... :l ,,_
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Table 2: Advantages and Disadvantag
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trend for many companies to reduce
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fluxes through a particular control
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known as a casting, is usually ejec
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Table 3: Prototyping Technology Mat
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quite accuratc for a testing level.
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For given values ofJ, Fn, Rn, En, t
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propeller geometry for impon into t
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Using OpenPVL_SW I a propeller desi
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o ...n".... 'Co 'OJ • • • DC)
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3.3 Simulations using CosmosFloWork
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simulation domain are set to 6m and
- Page 79: CosmosWorks can be used to check th
- Page 82: Figure 33: Dynamic Pressure Distrib
- Page 88: Chapter 4 Case Study: Simulation of
- Page 94 and 95: The plots of RPM and thrust from ou
- Page 96 and 97: Figure 46: Surface Dynamic Pressure
- Page 98: Figure 48: Deflection ofthe AUV Pro
- Page 102: In this simulation, two nose cones
- Page 110 and 111: Chapter 6 Propeller Fabrication by
- Page 112 and 113: Figure 60: Stratasys rDM 2000 After
- Page 115 and 116: Material options for Stratasys Fusi
- Page 117 and 118: Chapter 7 Conclusions and Future Wo
- Page 119 and 120: References III Burtner, E., 1953, "
- Page 121 and 122: [20] D'Epagnier, P.K., 2005, "A Com
- Page 123 and 124: Appendix 1\: The Part ofOpcnPVL_SW
- Page 125: Create all of the function commands
- Page 133 and 134: Set swSketehPt( 29 ) :=:: swModcl.C