Turbo Machinery Dynamics Part 9 pot

... Philadelphia, Pa., pp. 82 95 , 199 6. Chen, J. J., and Menq, C. H., “Periodic response of blades having three-dimensional non-linear shroud constraints,” ASME Paper # 99 -GT-2 89, New York, 199 9. Cheruvu, N. ... blades,” ASME Paper # 97 -GT-425, New York, 199 7. Chiang, H. D., and Kielb, R. E., “An analysis system for blade forced response,” ASME Journal of Turbo- Machinery 115:762–770,...

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... / 336 9. 6. NO x Formation / 340 9. 7. Effects of Swirl / 342 9. 8. Dry Low NO x Combustion System / 345 9. 9. Catalytic Combustor for Utility Turbine / 3 49 9.10. Acoustic Resonance / 351 9. 11. Active ... 314 Chapter 9. Combustion System 317 9. 1. Introduction / 317 9. 2. Fuels for Various Applications / 3 19 9.3. Combustion Principles / 324 9. 4. Combustor Designs and Selection...

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... 164, 214, 258 instability growth rate, 49 instability, baroclinic, 18, 97 , 164, 178, 182, 188, 199 , 258, 262, 271, 272 instability, barotropic, 87, 93 , 94 , 99 , 102, 164, 187, 258, 262 instability, ... eddy, 18, 19, 66, 164, 192 , 206, 2 59, 275 mixed layer, 214 mixing, 91 , 107, 214 mixing layer, 95 mixing length, 238, 242 mixing ratio, 25 momentum equation, 24, 66, 100, 1 19, 1...

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... vol. II, 198 1. Jahnsen, W., Peters, T., and Fottner, L., “Stall inception in a 5-stage hp compressor with increased load due to inlet distortions,” ASME Paper # 99 -GT-440, New York, 199 9. Kotidis, ... compressor,” ASME Paper # 91 -GT-88, New York, 199 1. Patterson, R. W., “Turbofan forced mixer-nozzle internal flow field i—A benchmark experimental study,” NASA CR 3 492 , 198 2. Pratt &am...

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... practice, damage mechanism,” EPRI 2, 199 9(b). Ragland, T. L., “Industrial gas turbine performance up-rates: Tips, tricks and traps,” ASME Paper # 97 -GT-4 09, New York, 199 7. Southall, L., and McQuiggan, ... load (MW) (MW) Fogging 71 8 793 160.5 53.6 7.0 207.1 Fog + chill 50 86 39 176.2 54.6 9. 2 221.6 Chilling 50 86 39 176.2 54.6 9. 4 221.4 No cooling 116 95 60 127.3 48.7 6.7 1 69....

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... three lobes (Heisler, 199 5). FIGURE 5.5 Screw type compressor (Heisler, 199 5). Kaya, H., “Catalytic combustion technologies,” Journal of Gas Turbine Society of Japan 25 (98 ): 48–51, 199 7. Nagaraj, B., ... com- pressor with pressure ratio of 23.3:1 for the LM2500+ gas turbine,” ASME Paper # 199 9-GT-210, New York, 199 9. Yee, R., Myers, L., Braccio, K., and Dvornak, M., “Enhanced TF40B gas...

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... speed (Day et al., 199 7). Time, rotor revolutions Pressure at 8 circumferential positions 10 × rotor frequency FIGURE 6. 19 Localized spike stall inception in SNECMA compressor (Day et al., 199 7). FIGURE ... in a low- speed compressor at the Whittle Laboratory of Cambridge University (Camp, 199 7; Camp and Day, 199 7). In high-speed machines experimental studies of this nature are difficul...

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... compressors,” ASME Paper # 91 -GT-87, New York, 199 1. Day, I. J., and Freeman C., “The unstable behavior of low and high speed compressors,” ASME Journal of Turbo- Machinery 116: 194 –201, 199 4. Ehrich, F. F., ... 0.54 0.56 0.58 0.60 0.86 0.88 0 .90 0 .92 0 .94 0 .96 Flow coefficient FIGURE 6.50 LM2500+ gas turbine high-pressure compressor improvements (Wadia, Wolf, and Haaser, 199...

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... Braembussche, 199 8). FIGURE 7.11 Streamlines at volute tongue (left), downstream of tongue (right) (Hillewaert and Van den Braembussche, 199 8). (Miner, Flack, and Allaire, 199 2), or through unsteady potential ... Palazzolo, 199 9). The development of radial gas turbines is described exhaustively by Mowill and Strom ( 198 3) and by Hiett and Johnston ( 196 4). Radial inflow turbine efficie...

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