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The original OpenPVL code is available at http://web.mil.edulopenprop/www/Download.html. The idea of this OpenPVL SW code is usc Solidworks to instead of Rihno with the same calculation methods. Based on this, replace all ofthe "rihno" words with "Solidworks" in the original code, whieh includes: Make rihno nag-o-I changes to Makc Slidworks nag 1 in Matlab code line 727 Geometry ( ..Make rihno nag...) changl.'S to Geometry ( ..Make Solidworks nag...) in Matlab code line 730 Function I) Geometry (...Make rihno nag...) changes to Function [I Geometry (...Make Solidworks nag...) in Matlab code line 1217 Thc part ofMatlab code to generate a propeller blade in Solidworks is integrated in the Mallab code line 1514 to instead ofRihno code. The logic nowchart ofthis solidworks eode displays as below: 112
Create all of the function commands at the beginning ofthe solidworks macro Use the calculation results in the original OpenPVL and sketch the first foil section, which is located at the root ofthe blade. (gct points first and then bspline connect all ofthe points) Sketch all the other foil sections in the order of from root to tip ofthe propeller blade. Connect all the points, which are located in the leading edge line to be as a reference line for lofting future Selecting all the foil sections and the reference line to loft them to generate a propeller bladc Hide all the points and curves for nice look 113
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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
Page 75 and 76: 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: Appendix 1\: The Part ofOpcnPVL_SW
Page 131: Appendix B: SolidWorks Macro lor th
Page 134: 'create loft swModcl.ClearSelcction
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