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14 FIGURE 5-22: MFP OPERARING RANGE IN THE MOC. ............................................................................. 157 FIGURE 5-23: COMPARISON BETWEEN PREDICTED AND MEASURED MFR FOR TURBINE A. .................. 158 FIGURE 5-24: DEVIATION BETWEEN PREDICTED AND MEASURED MFR FOR TURBINE A. ....................... 159 FIGURE 5-25: COMPARISON BETWEEN PREDICTED AND MEASURED 𝜂𝑡𝑠 FOR TURBINE A. .................... 160 FIGURE 5-26: DEVIATION BETWEEN PREDICTED AND MEASURED 𝜂𝑡𝑠 FOR TURBINE A.......................... 160 FIGURE 5-27: COMPARISON BETWEEN PREDICTED AND MEASURED 𝜂𝑡𝑠 FOR TURBINE B. .................... 161 FIGURE 5-28: COMPARISON BETWEEN PREDICTED AND MEASURED 𝑊𝑜𝑢𝑡 FOR TURBINE B. ................ 162 FIGURE 5-29: DEVIATION BETWEEN PREDICTED ANDMEASURED 𝜂𝑡𝑠 AND 𝑊𝑜𝑢𝑡 FOR TURBINE B........162 FIGURE 5-30: PERFORMANCE OF TURBINE B UNDER WIDE RANGE OF OPERATING CONDITIONS USING MOC. ................................................................................................................................................ 163 FIGURE 5-31: MFR OF TURBINE B UNDER WIDE RANGE OF OPERATING CONDITIONS USING MOC....... 164 FIGURE 5-32: COMPARISON BETWEEN PREDICTED AND MEASURED 𝜂𝑡𝑡FOR TURBINE C. ..................... 165 FIGURE 6-1: VOLUTE AREA AND RADIUS AT EACH AZIMUTH ANGLE. ..................................................... 170 FIGURE 6-2: 3D MODEL OF THE VOLUTE.................................................................................................. 170 FIGURE 6-3: CONNECTION PIPE BETWEEN THE VOLUTE AND THE EVAPORATOR. .................................. 171 FIGURE 6-4: 3D MODEL OF THE STATOR. ................................................................................................. 171 FIGURE 6-5: 2D MERIDIONAL PROFILES OF THE TURBINE BLADE. ........................................................... 172 FIGURE 6-6: CONSTRUCTION OF THE MERIDIONAL PROFILES. ................................................................ 173 FIGURE 6-7: BLADE ANGLE DISTRIBUTION AT HUB AND SHROUD OF THE ROTOR BLADE. ..................... 175 FIGURE 6-8: 3D MODEL OF THE TURBINE ROTOR. ................................................................................... 176 FIGURE 6-9: STEPS FOR CFD SIMULATION USING ANSYS......................................................................... 177 FIGURE 6-10: STATOR MESH OF 5.6 X 105 NODES USING ANSYS (TOP) HUB REGION AND (BOTTOM) 3D MESH. ............................................................................................................................................... 181 FIGURE 6-11: ROTOR MESH OF 5.9 X 105 NODES USING ANSYS (TOP) TIP REGION AND (BOTTOM) 3D MESH. ............................................................................................................................................... 181 FIGURE 6-12: MESH INDEPENDENCE STUDY USING ANSYS TURBOGRID. ................................................ 182 FIGURE 6-13: COMPUTATIONAL FLUID DOMAINS FOR STATOR AND ROTOR. ........................................ 183 FIGURE 6-14: RESIDUAL PLOTS FOR MOMENTUM AND MASS (TOP), AND MASS FLOW DIFFERENCE BWTEEN TURBINE INLET AND EXIT (BOTTOM). ............................................................................... 184 FIGURE 6-15: PRESSURE AND TEMPERATURE DISTRIBUTIONS AT DESIGN POINT (N=40,000 RPM, PR=6.9). .......................................................................................................................................................... 185 FIGURE 6-16: MACH NUMBER DISTRIBUTION AT DESIGN POINT (N=40,000 RPM, PR=6.9).................... 185 FIGURE 6-17: BLADE LOADING THROUGH THE ROTOR BLADES. ............................................................. 186 FIGURE 6-18: VELOCITY STREAMLINE AT 50% SPAN (TOP) AND 90% SPAN (BOTTOM), AT DESIGN POINT (N=40,000 RPM, PR=6.9). ................................................................................................................. 186PDF Image | Automotive Radial Turbine Expander Design WHR
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