Gas turbine theory:
Gespeichert in:
| Hauptverfasser: | , , |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Harlow [u.a.]
Prentice Hall
2001
|
| Ausgabe: | 5. ed. |
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | Bis 4. Aufl. u.d.T.: Cohen, Henry: Gas turbine theory |
| Beschreibung: | XVI, 491 S. Ill., graph. Darst. |
| ISBN: | 013015847X |
Internformat
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| 100 | 1 | |a Saravanamuttoo, H. I. |e Verfasser |4 aut | |
| 245 | 1 | 0 | |a Gas turbine theory |c H. I. H. Saravanamuttoo ; G. F. C. Rogers ; H. Cohen |
| 250 | |a 5. ed. | ||
| 264 | 1 | |a Harlow [u.a.] |b Prentice Hall |c 2001 | |
| 300 | |a XVI, 491 S. |b Ill., graph. Darst. | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 500 | |a Bis 4. Aufl. u.d.T.: Cohen, Henry: Gas turbine theory | ||
| 650 | 7 | |a Gasmotoren |2 gtt | |
| 650 | 7 | |a Turbinas a gás |2 larpcal | |
| 650 | 7 | |a Turbines |2 gtt | |
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| 700 | 1 | |a Rogers, G. F. C. |e Verfasser |4 aut | |
| 700 | 1 | |a Cohen, Henry |e Verfasser |4 aut | |
| 856 | 4 | 2 | |m HBZ Datenaustausch |q application/pdf |u http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015190795&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |3 Inhaltsverzeichnis |
| 999 | |a oai:aleph.bib-bvb.de:BVB01-015190795 | ||
Datensatz im Suchindex
| _version_ | 1804135947941445632 |
|---|---|
| adam_text | Titel: Gas turbine theory
Autor: Saravanamuttoo, Herbert I. H
Jahr: 2001
Contents
Prefaces ix
1 Introduction 1
1.1 Open-cycle single-shaft and twin-shaft arrangements 6
1.2 Multi-spool arrangements 9
1.3 Closed cycles 10
1.4 Aircraft propulsion 12
1.5 Industrial applications 18
1.6 Marine and land transportation 28
1.7 Environmental issues 32
1.8 Some future possibilities 34
1.9 Gas turbine design procedure 38
2 Shaft power cycles 45
2.1 Ideal cycles 45
2.2 Methods of accounting for component losses 53
2.3 Design point performance calculations 73
2.4 Comparative performance of practical cycles 81
2.5 Combined cycles and cogeneration schemes 89
2.6 Closed-cycle gas turbines 93
3 Gas turbine cycles for aircraft propulsion 99
3.1 Criteria of performance - 100
3.2 Intake and propelling nozzle efficiencies 104
3.3 Simple turbojet cycle 113
3.4 The turbofan engine 121
3.5 The turboprop engine 136
3.6 The turboshaft engine 139
3.7 Auxiliary Power Units 140
3.8 Thrust augmentation 142
3.9 Miscellaneous topics 145
152
154
162
167
172
175
179
181
182
185
188
193
195
198
207
228
238
246
252
255
262
264
265
266
268
270
275
283
290
301
305
305
322
328
345
355
356
366
Centrifugal compressors
4.1 Principle of operation
4.2 Work done and pressure rise
4.3 The diffuser
4.4 Compressibility effects
4.5 Non-dimensional quantities for plotting compressor
characteristics
4.6 Compressor characteristics
4.7 Computerized design procedures
Axial flow compressors
5.1 Basic operation
5.2 Elementary theory
5.3 Factors affecting stage pressure ratio
5.4 Blockage in the compressor annulus
5.5 Degree of reaction
5.6 Three-dimensional flow
5.7 Design process
5.8 Blade design
5.9 Calculation of stage performance
5.10 Compressibility effects
5.11 Off-design performance
5.12 Axial compressor characteristics
5.13 Closure
Combustion systems
6.1 Operational requirements
6.2 Types of combustion system
6.3 Some important factors affecting combustor design
6.4 The combustion process
6.5 Combustion chamber performance
6.6 Some practical problems
6.7 Gas turbine emissions
6.8 Coal gasification
Axial and radial flow turbines
7.1 Elementary theory of axial flow turbine
7.2 Vortex theory
7.3 Choice of blade profile, pitch and chord
7.4 Estimation of stage performance
7.5 Overall turbine performance
7.6 The cooled turbine
7.7 The radial flow turbine
CONTENTS vii
8 Prediction of performance of simple gas turbines 374
8.1 Component characteristics 376
8.2 Off-design operation of the single-shaft gas turbine 378
8.3 Equilibrium running of a gas generator 383
8.4 Off-design operation of free turbine engine 386
8.5 Off-design operation of the jet engine 397
8.6 Methods of displacing the equilibrium running line 405
8.7 Incorporation of variable pressure losses 409
9 Prediction of performance—further topics 411
9.1 Methods of improving part-load performance 411
9.2 Matching procedures for twin-spool engines 416
9.3 Some notes on the behaviour of twin-spool engines 421
9.4 Matching procedures for turbofan engines 425
9.5 Transient behaviour of gas turbines 427
9.6 Performance deterioration 435
9.7 Principles of control systems 438
Appendix A Some notes on gas dynamics 443
A.l Compressibility effects (qualitative treatment) 443
A.2 Basic equations for steady one-dimensional compressible
flow of a perfect gas in a duct 447
A.3 Isentropic flow in a duct of varying area 449
A.4 Frictionless flow in a constant area duct with heat transfer 451
A.5 Adiabatic flow in a constant area duct with friction 452
A.6 Plane normal shock waves 454
A.7 Oblique shock waves 458
A.8 Isentropic two-dimensional supersonic expansion and
compression 461
Appendix B Problems 463
Appendix C References 475
Index
483
|
| adam_txt |
Titel: Gas turbine theory
Autor: Saravanamuttoo, Herbert I. H
Jahr: 2001
Contents
Prefaces ix
1 Introduction 1
1.1 Open-cycle single-shaft and twin-shaft arrangements 6
1.2 Multi-spool arrangements 9
1.3 Closed cycles 10
1.4 Aircraft propulsion 12
1.5 Industrial applications 18
1.6 Marine and land transportation 28
1.7 Environmental issues 32
1.8 Some future possibilities 34
1.9 Gas turbine design procedure 38
2 Shaft power cycles 45
2.1 Ideal cycles 45
2.2 Methods of accounting for component losses 53
2.3 Design point performance calculations 73
2.4 Comparative performance of practical cycles 81
2.5 Combined cycles and cogeneration schemes 89
2.6 Closed-cycle gas turbines 93
3 Gas turbine cycles for aircraft propulsion 99
3.1 Criteria of performance - 100
3.2 Intake and propelling nozzle efficiencies 104
3.3 Simple turbojet cycle 113
3.4 The turbofan engine 121
3.5 The turboprop engine 136
3.6 The turboshaft engine 139
3.7 Auxiliary Power Units 140
3.8 Thrust augmentation 142
3.9 Miscellaneous topics 145
152
154
162
167
172
175
179
181
182
185
188
193
195
198
207
228
238
246
252
255
262
264
265
266
268
270
275
283
290
301
305
305
322
328
345
355
356
366
Centrifugal compressors
4.1 Principle of operation
4.2 Work done and pressure rise
4.3 The diffuser
4.4 Compressibility effects
4.5 Non-dimensional quantities for plotting compressor
characteristics
4.6 Compressor characteristics
4.7 Computerized design procedures
Axial flow compressors
5.1 Basic operation
5.2 Elementary theory
5.3 Factors affecting stage pressure ratio
5.4 Blockage in the compressor annulus
5.5 Degree of reaction
5.6 Three-dimensional flow
5.7 Design process
5.8 Blade design
5.9 Calculation of stage performance
5.10 Compressibility effects
5.11 Off-design performance
5.12 Axial compressor characteristics
5.13 Closure
Combustion systems
6.1 Operational requirements
6.2 Types of combustion system
6.3 Some important factors affecting combustor design
6.4 The combustion process
6.5 Combustion chamber performance
6.6 Some practical problems
6.7 Gas turbine emissions
6.8 Coal gasification
Axial and radial flow turbines
7.1 Elementary theory of axial flow turbine
7.2 Vortex theory
7.3 Choice of blade profile, pitch and chord
7.4 Estimation of stage performance
7.5 Overall turbine performance
7.6 The cooled turbine
7.7 The radial flow turbine
CONTENTS vii
8 Prediction of performance of simple gas turbines 374
8.1 Component characteristics 376
8.2 Off-design operation of the single-shaft gas turbine 378
8.3 Equilibrium running of a gas generator 383
8.4 Off-design operation of free turbine engine 386
8.5 Off-design operation of the jet engine 397
8.6 Methods of displacing the equilibrium running line 405
8.7 Incorporation of variable pressure losses 409
9 Prediction of performance—further topics 411
9.1 Methods of improving part-load performance 411
9.2 Matching procedures for twin-spool engines 416
9.3 Some notes on the behaviour of twin-spool engines 421
9.4 Matching procedures for turbofan engines 425
9.5 Transient behaviour of gas turbines 427
9.6 Performance deterioration 435
9.7 Principles of control systems 438
Appendix A Some notes on gas dynamics 443
A.l Compressibility effects (qualitative treatment) 443
A.2 Basic equations for steady one-dimensional compressible
flow of a perfect gas in a duct 447
A.3 Isentropic flow in a duct of varying area 449
A.4 Frictionless flow in a constant area duct with heat transfer 451
A.5 Adiabatic flow in a constant area duct with friction 452
A.6 Plane normal shock waves 454
A.7 Oblique shock waves 458
A.8 Isentropic two-dimensional supersonic expansion and
compression 461
Appendix B Problems 463
Appendix C References 475
Index
483 |
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| illustrated | Illustrated |
| index_date | 2024-07-02T16:09:41Z |
| indexdate | 2024-07-09T20:48:36Z |
| institution | BVB |
| isbn | 013015847X |
| language | English |
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| physical | XVI, 491 S. Ill., graph. Darst. |
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| publisher | Prentice Hall |
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| spelling | Saravanamuttoo, H. I. Verfasser aut Gas turbine theory H. I. H. Saravanamuttoo ; G. F. C. Rogers ; H. Cohen 5. ed. Harlow [u.a.] Prentice Hall 2001 XVI, 491 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier Bis 4. Aufl. u.d.T.: Cohen, Henry: Gas turbine theory Gasmotoren gtt Turbinas a gás larpcal Turbines gtt Gas-turbines Gasturbine (DE-588)4019416-4 gnd rswk-swf Gasturbine (DE-588)4019416-4 s DE-604 Rogers, G. F. C. Verfasser aut Cohen, Henry Verfasser aut HBZ Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015190795&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Saravanamuttoo, H. I. Rogers, G. F. C. Cohen, Henry Gas turbine theory Gasmotoren gtt Turbinas a gás larpcal Turbines gtt Gas-turbines Gasturbine (DE-588)4019416-4 gnd |
| subject_GND | (DE-588)4019416-4 |
| title | Gas turbine theory |
| title_auth | Gas turbine theory |
| title_exact_search | Gas turbine theory |
| title_exact_search_txtP | Gas turbine theory |
| title_full | Gas turbine theory H. I. H. Saravanamuttoo ; G. F. C. Rogers ; H. Cohen |
| title_fullStr | Gas turbine theory H. I. H. Saravanamuttoo ; G. F. C. Rogers ; H. Cohen |
| title_full_unstemmed | Gas turbine theory H. I. H. Saravanamuttoo ; G. F. C. Rogers ; H. Cohen |
| title_short | Gas turbine theory |
| title_sort | gas turbine theory |
| topic | Gasmotoren gtt Turbinas a gás larpcal Turbines gtt Gas-turbines Gasturbine (DE-588)4019416-4 gnd |
| topic_facet | Gasmotoren Turbinas a gás Turbines Gas-turbines Gasturbine |
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