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Appendix Symbols AA incremental spanwise flow area, cm 2 r cp specific heat of air at constant pressure r/rr B NP NS number number of of impeller blade passages spanwise survey locations axial velocity component, m/sec tangential velocity component, relative velocity, m/sec m/sec; I_m "gin m/sec unit vector in the nth measured velocity component direction unit vector in local meridional grid direction unit vector in local pitchwise grid direction, 0 SS s T t tstd V vl vT Vo W unit vector in local spanwise grid direction g,st unit vector in local streamwise grid direction sea-level conditions; i ith static tap J streamwise measurement grid index velocity components in x-, y-, and z-coordinate direc- tions, m/sec absolute velocity, m/sec velocity component measured in direction -fn' m/sec meridional velocity component, rrdsec; _z 2 + Vr2 rh mass flow rate, kg/sec rhd design mass flow rate; 30.0 kg/sec m/ms nondimensional shroud meridional distance N rotor rotational speed, rad/sec NM number tions of laser anemometer measurement at a given window realiza- radial velocity throughflow component, m/sec velocity component, NWN number windows rotor relative pitchwise measurement NZ number of measurements w,, nth rotor relative pitchwise laser anemometer meas- urement window % pitchwise secondary velocity component, m/sec secondary velocity vector, m/sec; l_'- I_'st spanwise secondary velocity component (positive towards the shroud), m/sec vector projection of I_' in the local streamwise direction gst, m/sec P PS total pressure pressure surface of rotor blade passages with zero P static pressure Pstd pressure at standard-day sea-level conditions; 101 325 N/m 2 R 14 universal gas constant for air radial coordinate, cm radius nondimensionalized suction surface surface distance total temperature static temperature temperature at standard-day 288.15 K impeller tip speed, m/sec by exit tip radius WO relative tangential velocity component, m/secPDF Image | Laser anemometer measurements of the three-dimensional rotor flow
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