Heat transfer in gas turbine systems:
Gespeichert in:
| Format: | Buch |
|---|---|
| Sprache: | English |
| Veröffentlicht: |
New York, NY
New York Acad. of Sciences
2001
|
| Schriftenreihe: | Annals of the New York Academy of Sciences
934 |
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | XI, 522 S. Ill., graph. Darst. |
| ISBN: | 1573313289 1573313297 |
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Datensatz im Suchindex
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| adam_text | ANNALS OF THE NEW YORK ACADEMY OF SCIENCES
Volume 934
May 2001
HEAT TRANSFER IN GAS
TURBINE SYSTEMS
Editor
Richard J. Goldstein
[This volume is the result of a conference entitled Turbine 2000: International Symposium
on Heat Transfer in Gas Turbine Systems sponsored by the International Centre for Heat
and Mass Transfer (ICHMT) on August 13 18, 2000, in Cesme, Izmir, Turkey.]
CONTENTS
Preface. By R. J. GOLDSTEIN xi
Synopsis. By V. Srinivasan, T. W. Simon, and R. J. Goldstein 1
Invited Papers
Secondary Flows in Axial Turbines—A Review. By L. S. Langston 11
Heat Transfer near Turbine Nozzle Endwall. By M. K. Chyu 27
Transition to Turbulence under Low Pressure Turbine Conditions.
By T. W. Simon and R. W. Kaszeta 37
Turbulence Modeling in Simulation of Gas Turbine Flow and Heat Transfer.
By G. Brereton and T. I P. Shih 52
A Review of Turbine Blade Tip Heat Transfer. By R. S. Bunker 64
Unsteady Flow Modelling in Turbine Stage. By F. MARTELLI 80
The Detailed Structure and Behavior of Discrete Cooling Jets in a Turbine.
By F. Leboeuf and O. Sgarzi 95
Flow and Heat Transfer Predictions for Film Cooling. By S. ACHARYA,
M. Tyagi, and A. Hoda 110
Film Cooling: What Did We Learn from Our Measurements? By T. Arts 126
Combustor Liner Cooling Technology in Scope of Reduced Pollutant
Formation and Rising Thermal Efficiencies. By A. SCHULZ 135
Jet Impingement Heat Transfer in Gas Turbine Systems. By B. HAN AND
R. J. Goldstein 147
Recent Developments in Turbine Blade Internal Cooling. By J C. Han AND
S. Dutta 162
Heat Transfer Technology for Internal Passages of Air Cooled Blades for
Heavy Duty Gas Turbines. By B. Weigand, K. Semmler, AND
J. VON WOLFERSDORF 179
Cooling Systems for Ultra High Temperature Turbines. By T. YOSHIDA 194
Some Current Research in Rotating Disc Systems. By J. M. OWEN AND
M. Wilson 206
Selection of a Turbine Cooling System Applying Multidisciplinary Design
Considerations. By B. Glezer 222
Contributed Papers
Analysis of Particle Laden Flow and Heat Transfer in Cascade and Rocket
Nozzle. By H. H. Cho, W. S. Kim, M. S. Yu, and J. C. Bae 233
Convective Heat Transfer on an Inlet Guide Vane. By M L. HOLMER,
L E. Eriksson, and B. Sunden 241
Effect of Reynolds Number, Turbulence Level, and Periodic Wake Flow on
Heat Transfer on Low Pressure Turbine Blades. By D. Suslov,
A. SCHULZ, AND S. WlTTIG 249
Surface Temperature Mapping of Gas Turbine Blading by Means of
High Resolution Pyrometry. By S. L. F. Frank 257
Studies on Free Stream Turbulence as Related to Gas Turbine Heat Transfer:
A Review of Authors Past Work and Future Implications. By
S. Yavuzkurt and G. R. Iyer 265
A Conjugate Heat Transfer Procedure for Gas Turbine Blades. By G. CROCE... 273
Heat/Mass Transfer Characteristics on Turbine Shroud with Blade Tip
Clearance. By H. H. CHO, D. H. Rhee, and J. H. CHOI 281
Heat Transfer and Flow Characteristics on a Gas Turbine Shroud.
By M. Obata, M. Kumada, and N. Ijichi 289
A Novel Digital Image Processing System for the Transient Liquid Crystal
Technique Applied for Heat Transfer and Film Cooling Measurements.
By G. VOGEL AND A. BOELCS 297
Contribution of Heat Transfer to Turbine Blades and Vanes for High
Temperature Industrial Gas Turbines: Part 1. Film Cooling.
By K I. Takeishi and S. Aoki 305
Experimental Investigation of Film Cooling Flow Induced by Shaped Holes
on a Turbine Blade. By S. Barthet and F. Bario 313
Film Cooling from Rows of Holes—Effect of Cooling Hole Shape and Row
Arrangement on Adiabatic Effectiveness. By J. Dittmar, I. S. Jung,
A. SCHULZ, S. WlTTIG, AND J. S. LEE 321
Effects of Bulk Flow Pulsations on Film Cooling with Shaped Holes. By
H W. Lee and J. S. Lee 329
Film Cooling: Case of Double Rows of Staggered Jets. By E. DORIGNAC, J. J.
VULLIERME, P. NOIRAULT, E. FOUCAULT, AND J. L. BOUSGARBIES . . . 337
Characteristics of Various Film Cooling Jets Injected in a Conduit.
ByH. Takahashi, C. Nuntadusit, H. Kimoto, H. Ishida, T. Ukai,
and K I. Takeishi 345
Film Cooling Performance on Curved Walls with Compound Angle Hole
Configuration. By P H. Chen, M S. Hung, and P P. Ding 353
The Variation of Heat Transfer Coefficient, Adiabatic Effectiveness, and
Aerodynamic Loss with Film Cooling Hole Shape. By J. E. Sargison,
S. M. Guo, M. L. G. Oldfield, and A. J. Rawlinson 361
Numerical Investigation of Film Cooling Flow Induced by Cylindrical and
Shaped Holes. By S. Barthet and P. Kulisa 369
Numerical Investigation of Heat Transfer on Film Cooled Turbine Blades.
By P. Ginibre, M. Lefebvre, and N. Liamis 377
Comparison between Two Models of Cooling Surfaces Using Blowing.
By L. Mathelin, F. Bataille, and A. Lallemand 385
Finite Element Analysis of Flow Field in the Single Hole Film Cooling
Technique. By F. Bazdidi Tehrani and A. A. Mahmoodi 393
Effects of Entrance Cross Flow Directions to Film Cooling Holes.
By C. Saumweber, A. Schulz, S. Wittig, and M. Gritsch 401
Mach Number Effect on Jet Impingement Heat Transfer. By P. Brevet,
E. DORIGNAC, AND J. J. VULLIERME 409
Numerical Investigation of Combined Impingement and Convection Heat
Transfer. By A. ABDON AND B. Sunden 417
Mass/Heat Transfer in Dimpled Two Pass Coolant Passages with Rotation.
By F. Zhou and S. Acharya 424
Detailed Heat/Mass Transfer Distributions in a Rotating Two Pass Coolant
Channel with Engine Near Cross Section and Smooth Walls.
By L. Rathjen, d. K. Hennecke, S. Bock, and R. Kleinstuck 432
Analyses of Heat Transfer in Stationary and Rotating Ribbed Blade Cooling
Passages Using Computational Fluid Dynamics. By R. A. BREWSTER
AND S. JONNAVITHULA 440
Prediction of Pressure Loss and Heat Transfer in Internal Cooling Passages.
By K. HERMANSON, S. PARNEIX, J. VON WOLFERSDORF, AND
K. SEMMLER 448
Numerical Simulation of Local Heat Transfer in Rotating Two Pass Square
Channels. By A. I. Kirillov, V. V. RlS, E. M. SMIRNOV, AND
D. K. Zaitsev 456
Experimental Determination of Average Turbulent Heat Transfer and Friction
Factor in Stator Internal Rib Roughened Cooling Channels. By
L. Battisti and P. Baggio 464
Contribution of Heat Transfer to Turbine Blades and Vanes for High
Temperature Industrial Gas Turbines: Part 2. Heat Transfer on
Serpentine Flow Passage. By K I. TAKEISHI AND S. Aoki 473
Secondary Flow Effect to Heat Transfer of a Duct with Discrete Rib
Turbulators. By K. Tatsumi, H. Iwai, K. Inaoka, and K. Suzuki ... 481
Development of Nondestructive Inspection Method for the Performance of
Thermal Barrier Coating. By M. Morinaga and T. Takahashi 489
Numerical Modelling of Flow and Heat Transfer in the Rotating Disc Cavities
of a Turboprop Engine. By J. Faragher and A. Ooi 497
Verifying Heat Transfer Analysis of High Pressure Cooled Turbine Blades
and Disk. By S. Yamawaki 505
Computation of Flow and Heat Transfer in Rotating Cavities with Peripheral
Flow of Cooling Air. By M. Kiliq 513
Index of Contributors 521
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| spelling | Heat transfer in gas turbine systems ed. by Richard J. Goldstein ... New York, NY New York Acad. of Sciences 2001 XI, 522 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier Annals of the New York Academy of Sciences 934 Chaleur - Transmission - Congrès Gasturbines gtt Turbines à gaz - Congrès Warmtetransport gtt Calorimetry Gas-turbines Heat Transmission Technology Gasturbine (DE-588)4019416-4 gnd rswk-swf Wärmeübertragung (DE-588)4064211-2 gnd rswk-swf (DE-588)1071861417 Konferenzschrift 2000 Çeşme gnd-content Gasturbine (DE-588)4019416-4 s Wärmeübertragung (DE-588)4064211-2 s DE-604 Goldstein, Richard J. Sonstige oth Annals of the New York Academy of Sciences 934 (DE-604)BV002532608 934 HBZ Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=009516706&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Heat transfer in gas turbine systems Annals of the New York Academy of Sciences Chaleur - Transmission - Congrès Gasturbines gtt Turbines à gaz - Congrès Warmtetransport gtt Calorimetry Gas-turbines Heat Transmission Technology Gasturbine (DE-588)4019416-4 gnd Wärmeübertragung (DE-588)4064211-2 gnd |
| subject_GND | (DE-588)4019416-4 (DE-588)4064211-2 (DE-588)1071861417 |
| title | Heat transfer in gas turbine systems |
| title_auth | Heat transfer in gas turbine systems |
| title_exact_search | Heat transfer in gas turbine systems |
| title_full | Heat transfer in gas turbine systems ed. by Richard J. Goldstein ... |
| title_fullStr | Heat transfer in gas turbine systems ed. by Richard J. Goldstein ... |
| title_full_unstemmed | Heat transfer in gas turbine systems ed. by Richard J. Goldstein ... |
| title_short | Heat transfer in gas turbine systems |
| title_sort | heat transfer in gas turbine systems |
| topic | Chaleur - Transmission - Congrès Gasturbines gtt Turbines à gaz - Congrès Warmtetransport gtt Calorimetry Gas-turbines Heat Transmission Technology Gasturbine (DE-588)4019416-4 gnd Wärmeübertragung (DE-588)4064211-2 gnd |
| topic_facet | Chaleur - Transmission - Congrès Gasturbines Turbines à gaz - Congrès Warmtetransport Calorimetry Gas-turbines Heat Transmission Technology Gasturbine Wärmeübertragung Konferenzschrift 2000 Çeşme |
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