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14 FIGURE β5-22: MFP OPERARING RANGE IN THE MOC. ............................................................................. 157 FIGURE β5-23: COMPARISON BETWEEN PREDICTED AND MEASURED MFR FOR TURBINE A. .................. 158 FIGURE β5-24: DEVIATION BETWEEN PREDICTED AND MEASURED MFR FOR TURBINE A. ....................... 159 FIGURE β5-25: COMPARISON BETWEEN PREDICTED AND MEASURED ππ‘π FOR TURBINE A. .................... 160 FIGURE β5-26: DEVIATION BETWEEN PREDICTED AND MEASURED ππ‘π FOR TURBINE A.......................... 160 FIGURE β5-27: COMPARISON BETWEEN PREDICTED AND MEASURED ππ‘π FOR TURBINE B. .................... 161 FIGURE β5-28: COMPARISON BETWEEN PREDICTED AND MEASURED πππ’π‘ FOR TURBINE B. ................ 162 FIGURE β5-29: DEVIATION BETWEEN PREDICTED ANDMEASURED ππ‘π AND πππ’π‘ FOR TURBINE B........162 FIGURE β5-30: PERFORMANCE OF TURBINE B UNDER WIDE RANGE OF OPERATING CONDITIONS USING MOC. ................................................................................................................................................ 163 FIGURE β5-31: MFR OF TURBINE B UNDER WIDE RANGE OF OPERATING CONDITIONS USING MOC....... 164 FIGURE β5-32: COMPARISON BETWEEN PREDICTED AND MEASURED ππ‘π‘FOR TURBINE C. ..................... 165 FIGURE β6-1: VOLUTE AREA AND RADIUS AT EACH AZIMUTH ANGLE. ..................................................... 170 FIGURE β6-2: 3D MODEL OF THE VOLUTE.................................................................................................. 170 FIGURE β6-3: CONNECTION PIPE BETWEEN THE VOLUTE AND THE EVAPORATOR. .................................. 171 FIGURE β6-4: 3D MODEL OF THE STATOR. ................................................................................................. 171 FIGURE β6-5: 2D MERIDIONAL PROFILES OF THE TURBINE BLADE. ........................................................... 172 FIGURE β6-6: CONSTRUCTION OF THE MERIDIONAL PROFILES. ................................................................ 173 FIGURE β6-7: BLADE ANGLE DISTRIBUTION AT HUB AND SHROUD OF THE ROTOR BLADE. ..................... 175 FIGURE β6-8: 3D MODEL OF THE TURBINE ROTOR. ................................................................................... 176 FIGURE β6-9: STEPS FOR CFD SIMULATION USING ANSYS......................................................................... 177 FIGURE β6-10: STATOR MESH OF 5.6 X 105 NODES USING ANSYS (TOP) HUB REGION AND (BOTTOM) 3D MESH. ............................................................................................................................................... 181 FIGURE β6-11: ROTOR MESH OF 5.9 X 105 NODES USING ANSYS (TOP) TIP REGION AND (BOTTOM) 3D MESH. ............................................................................................................................................... 181 FIGURE β6-12: MESH INDEPENDENCE STUDY USING ANSYS TURBOGRID. ................................................ 182 FIGURE β6-13: COMPUTATIONAL FLUID DOMAINS FOR STATOR AND ROTOR. ........................................ 183 FIGURE β6-14: RESIDUAL PLOTS FOR MOMENTUM AND MASS (TOP), AND MASS FLOW DIFFERENCE BWTEEN TURBINE INLET AND EXIT (BOTTOM). ............................................................................... 184 FIGURE β6-15: PRESSURE AND TEMPERATURE DISTRIBUTIONS AT DESIGN POINT (N=40,000 RPM, PR=6.9). .......................................................................................................................................................... 185 FIGURE β6-16: MACH NUMBER DISTRIBUTION AT DESIGN POINT (N=40,000 RPM, PR=6.9).................... 185 FIGURE β6-17: BLADE LOADING THROUGH THE ROTOR BLADES. ............................................................. 186 FIGURE β6-18: 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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