Page 337 - Fluid Mechanics and Thermodynamics of Turbomachinery
P. 337

Index 319
                          Optimum space-chord ratio  87 8      Radial flow turbines, Ch. 8
                          Optimum design selection (IFR turbines)  basic design of rotor  241 2
                            26 et seq.                           cantilever type 237 8
                          Overall performance                    criterion for number of vanes  253 6
                            compressor characteristic 18 20      cooled  271 2
                            turbine characteristic  18 20        effect of specific speed 267 8
                                                                 inward flow types  237 9
                                                                 Mach number relations 246 7
                          Pascal, unit of pressure  4
                                                                 nominal design point efficiency  242 6
                          Pelton wheel turbine 2, 3, 279, 280 90
                                                                 nozzle loss coefficients 247 8
                            energy losses  286
                                                                 optimum design selection  266 9
                            nozzle efficiency 287
                                                                 optimum flow considerations  248 et
                            overall efficiency 287 8
                                                                   seq.
                            speed control 284
                          Penstock  285                          rotor loss coefficients 248
                            diameter  286                        velocity triangles  238, 239
                          Perfect gas 16, 17                   Reaction
                                                                 blade  70 1
                          Performance characteristics of
                                                                 compressor stage  143 4, 172 3, 176
                            turbomachines  7
                                                                 effect on efficiency 107 8
                          Pitch-line analysis assumption
                                                                 fifty per cent  103
                            axial compressor  138 9
                                                                 true value  179
                            axial turbine  93
                          Polytropic index  38                   turbine stage 101 4, 290
                          Power coefficient  6, 18, 301           zero value  102 3
                          Prerotation, effect on performance  209 12  Reheat factor  40
                          Pressure head 4                      Relative eddy  214
                                                               Reynolds number
                          Pressure ratio limits of centripetal turbine
                                                                 critical value  67
                            269 71
                                                               Rotating stall  157
                          Pressure recovery factor 46
                                                                 cause  157 8
                          Pressure rise coefficient 45
                                                                 control  159 60
                          Primary dimensions  6
                          Profile losses in compressor blading  69  Rothalpy  29, 204 5
                          Profile thickness  56                 Royal Aircraft Establishment (RAE) 137
                          Propagating stall 64                 Royal Society  3
                          Pump:
                            centrifugal 7 9, 200, 201, 206 8, 218 9
                                                               Scroll  201, 290
                            efficiency 7
                                                               Second law of thermodynamics  23, 29
                            head increase 218 9
                                                               Secondary flow  64
                            inlet, optimum design 206 8
                                                                 losses 84 5
                            mixed flow  2, 9, 12
                            simplified impeller design  202       vorticity  64
                            supercavitating  14, 15            Secondary flows  193 5
                            vane angle  215 6                    gyroscope analogy  193
                                                                 overturning due to  194
                                                               Shroud  201, 238
                          Radial equilibrium                   Shape number 10
                            direct problem  179 80             SI units 3 4
                            equation, theory 169 et seq.       Similitude  6 et seq.
                            forced vortex  175 6               Slip:
                            free-vortex  171 5                   definition  214
                            general whirl distribution 176 9     factor  213 18
                          Radial flow  169                        in IFR turbines  248 50
                          Radial flow compressors and pumps, Ch. 7  velocity  214
   332   333   334   335   336   337   338   339   340   341   342