Gas turbine theory:
Gespeichert in:
| Vorheriger Titel: | Saravanamuttoo, H. I. H. Gas turbine theory |
|---|---|
| Format: | Buch |
| Sprache: | English |
| Veröffentlicht: |
Harlow, England ; Munich [u.a.]
Prentice Hall
2009
|
| Ausgabe: | 6. ed. |
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | Includes bibliographical references and index |
| Beschreibung: | XVI, 590 S. Ill., graph. Darst. |
| ISBN: | 9780132224376 |
Internformat
MARC
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| 020 | |a 9780132224376 |c cased |9 978-0-13-222437-6 | ||
| 035 | |a (OCoLC)232358227 | ||
| 035 | |a (DE-599)BVBBV035093667 | ||
| 040 | |a DE-604 |b ger |e aacr | ||
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| 245 | 1 | 0 | |a Gas turbine theory |c H.I.H. Saravanamuttoo ... [et al.] |
| 250 | |a 6. ed. | ||
| 264 | 1 | |a Harlow, England ; Munich [u.a.] |b Prentice Hall |c 2009 | |
| 300 | |a XVI, 590 S. |b Ill., graph. Darst. | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 500 | |a Includes bibliographical references and index | ||
| 650 | 4 | |a Gas-turbines | |
| 650 | 0 | 7 | |a Gasturbine |0 (DE-588)4019416-4 |2 gnd |9 rswk-swf |
| 689 | 0 | 0 | |a Gasturbine |0 (DE-588)4019416-4 |D s |
| 689 | 0 | |5 DE-604 | |
| 700 | 1 | |a Saravanamuttoo, H. I. |e Sonstige |4 oth | |
| 780 | 0 | 0 | |i Bis 5. Auflage |a Saravanamuttoo, H. I. H. |t Gas turbine theory |
| 856 | 4 | 2 | |m Digitalisierung UB Bayreuth |q application/pdf |u http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=016761742&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |3 Inhaltsverzeichnis |
| 999 | |a oai:aleph.bib-bvb.de:BVB01-016761742 | ||
Datensatz im Suchindex
| _version_ | 1804138051986784256 |
|---|---|
| adam_text | Contents
Foreword
vii
Prefaces
viii
Publisher s Acknowledgements
xvii
Introduction
1
1.1
Open-cycle single-shaft and twin-shaft arrangements
5
1.2
Multi-spool arrangements
9
1.3
Closed cycles
10
1.4
Aircraft propulsion
12
1.5
Industrial applications
20
1.6
Marine and land transportation
29
1.7
Environmental issues
34
1.8
Some future possibilities
36
1.9
Gas turbine design procedure
40
Shaft power cycles
46
2.1
Ideal cycles
46
2.2
Methods of accounting for component losses
54
2.3
Design point performance calculations
75
2.4
Comparative performance of practical cycles
84
2.5
Combined cycles and cogeneration schemes
89
2.6
Closed-cycle gas turbines
94
Gas turbine cycles for aircraft propulsion
100
3.1
Criteria of performance
101
3.2
Intake and propelling nozzle efficiencies
105
3.3
Simple turbojet cycle
114
3.4
The
turbofan
engine
123
3.5
The turboprop engine
139
3.6
The
turboshaft
engine
142
3.7
Auxiliary power units
143
3.8
Thrust augmentation
147
3.9
Miscellaneous topics
150
iv CONTENTS
4
Centrifugal
compressors
157
4.1
Principle of operation
158
4.2
Work done and pressure rise
160
4.3
The
diffuser
168
4.4
Compressibility effects
173
4.5
Non-dimensional quantities for plotting compressor
characteristics
178
4.6
Compressor characteristics
181
4.7
Computerized design procedures
185
5
Axial flow compressors
187
5.1
Basic operation
188
5.2
Elementary theory
191
5.3
Factors affecting stage pressure ratio
194
5.4
Blockage in the compressor annulus
199
5.5
Degree of reaction
201
5.6
Three-dimensional flow
204
5.7
Design process
213
5.8
Blade design
234
5.9
Calculation of stage performance
245
5.10
Compressibility effects
254
5.11
Off-design performance
259
5.12
Axial compressor characteristics
263
5.13
Closure
270
6
Combustion systems
272
6.1
Operational requirements
273
6.2
Types of combustion system
274
6.3
Some important factors affecting combustor design
277
6.4
The combustion process
278
6.5
Combustion chamber performance
283
6.6
Some practical problems
292
6.7
Gas turbine emissions
299
6.8
Coal gasification
311
7
Axial and radial flow turbines
315
7.1
Elementary theory of axial flow turbine
316
7.2
Vortex theory
334
7.3
Choice of blade profile, pitch and chord
341
7.4
Estimation of stage performance
354
7.5
Overall turbine performance
364
7.6
The cooled turbine
366
7.7
The radial flow turbine
376
8
Mechanical design of gas turbines
385
8.1
Design process
386
CONTENTS
V
8.2 Gas
turbine
architecture
388
8.3
Loads and failure modes
390
8.4
Gas turbine materials
392
8.5
Design against failure and life estimations
412
8.6
Blades
417
8.7
Bladed rotor discs
428
8.8
Blade and disc vibration
434
8.9
Engine vibration
440
8.10
Other components
445
8.11
Closure
451
9
Prediction of performance of simple gas turbines
453
9.1
Component characteristics
456
9.2
Off-design operation of the single-shaft gas turbine
457
9.3
Equilibrium running of a gas generator
463
9.4
Off-design operation of free turbine engine
466
9.5
Off-design operation of the jet engine
477
9.6
Methods of displacing the equilibrium running line
486
9.7
Incorporation of variable pressure losses
489
9.8
Power extraction
490
10
Prediction of performance
—
further topics
492
10.1
Methods of improving part-load performance
492
10.2
Matching procedures for twin-spool engines
497
10.3
Some notes on the behaviour of twin-spool engines
502
10.4
Matching procedures for
turbofan
engines
506
10.5
Transient behaviour of gas turbines
508
10.6
Performance deterioration
516
10.7
Principles of control systems
520
Appendix A Some notes on gas dynamics
525
A.
1
Compressibility effects (qualitative treatment)
525
A.2 Basic equations for steady one-dimensional compressible
flow of a perfect gas in a duct
530
A.3 Isentropic flow in a duct of varying area
533
A.4 Frictionless flow in a constant area duct with heat transfer
534
A.5 Adiabatic flow in a constant area duct with friction
536
A.6 Plane normal shock waves
538
A.7 Oblique shock waves
543
A.8 Isentropic two-dimensional supersonic expansion and
compression
547
Appendix
В
Problems
549
Appendix
С
References
568
Index
580
|
| adam_txt |
Contents
Foreword
vii
Prefaces
viii
Publisher's Acknowledgements
xvii
Introduction
1
1.1
Open-cycle single-shaft and twin-shaft arrangements
5
1.2
Multi-spool arrangements
9
1.3
Closed cycles
10
1.4
Aircraft propulsion
12
1.5
Industrial applications
20
1.6
Marine and land transportation
29
1.7
Environmental issues
34
1.8
Some future possibilities
36
1.9
Gas turbine design procedure
40
Shaft power cycles
46
2.1
Ideal cycles
46
2.2
Methods of accounting for component losses
54
2.3
Design point performance calculations
75
2.4
Comparative performance of practical cycles
84
2.5
Combined cycles and cogeneration schemes
89
2.6
Closed-cycle gas turbines
94
Gas turbine cycles for aircraft propulsion
100
3.1
Criteria of performance
101
3.2
Intake and propelling nozzle efficiencies
105
3.3
Simple turbojet cycle
114
3.4
The
turbofan
engine
123
3.5
The turboprop engine
139
3.6
The
turboshaft
engine
142
3.7
Auxiliary power units
143
3.8
Thrust augmentation
147
3.9
Miscellaneous topics
150
iv CONTENTS
4
Centrifugal
compressors
157
4.1
Principle of operation
158
4.2
Work done and pressure rise
160
4.3
The
diffuser
168
4.4
Compressibility effects
173
4.5
Non-dimensional quantities for plotting compressor
characteristics
178
4.6
Compressor characteristics
181
4.7
Computerized design procedures
185
5
Axial flow compressors
187
5.1
Basic operation
188
5.2
Elementary theory
191
5.3
Factors affecting stage pressure ratio
194
5.4
Blockage in the compressor annulus
199
5.5
Degree of reaction
201
5.6
Three-dimensional flow
204
5.7
Design process
213
5.8
Blade design
234
5.9
Calculation of stage performance
245
5.10
Compressibility effects
254
5.11
Off-design performance
259
5.12
Axial compressor characteristics
263
5.13
Closure
270
6
Combustion systems
272
6.1
Operational requirements
273
6.2
Types of combustion system
274
6.3
Some important factors affecting combustor design
277
6.4
The combustion process
278
6.5
Combustion chamber performance
283
6.6
Some practical problems
292
6.7
Gas turbine emissions
299
6.8
Coal gasification
311
7
Axial and radial flow turbines
315
7.1
Elementary theory of axial flow turbine
316
7.2
Vortex theory
334
7.3
Choice of blade profile, pitch and chord
341
7.4
Estimation of stage performance
354
7.5
Overall turbine performance
364
7.6
The cooled turbine
366
7.7
The radial flow turbine
376
8
Mechanical design of gas turbines
385
8.1
Design process
386
CONTENTS
V
8.2 Gas
turbine
architecture
388
8.3
Loads and failure modes
390
8.4
Gas turbine materials
392
8.5
Design against failure and life estimations
412
8.6
Blades
417
8.7
Bladed rotor discs
428
8.8
Blade and disc vibration
434
8.9
Engine vibration
440
8.10
Other components
445
8.11
Closure
451
9
Prediction of performance of simple gas turbines
453
9.1
Component characteristics
456
9.2
Off-design operation of the single-shaft gas turbine
457
9.3
Equilibrium running of a gas generator
463
9.4
Off-design operation of free turbine engine
466
9.5
Off-design operation of the jet engine
477
9.6
Methods of displacing the equilibrium running line
486
9.7
Incorporation of variable pressure losses
489
9.8
Power extraction
490
10
Prediction of performance
—
further topics
492
10.1
Methods of improving part-load performance
492
10.2
Matching procedures for twin-spool engines
497
10.3
Some notes on the behaviour of twin-spool engines
502
10.4
Matching procedures for
turbofan
engines
506
10.5
Transient behaviour of gas turbines
508
10.6
Performance deterioration
516
10.7
Principles of control systems
520
Appendix A Some notes on gas dynamics
525
A.
1
Compressibility effects (qualitative treatment)
525
A.2 Basic equations for steady one-dimensional compressible
flow of a perfect gas in a duct
530
A.3 Isentropic flow in a duct of varying area
533
A.4 Frictionless flow in a constant area duct with heat transfer
534
A.5 Adiabatic flow in a constant area duct with friction
536
A.6 Plane normal shock waves
538
A.7 Oblique shock waves
543
A.8 Isentropic two-dimensional supersonic expansion and
compression
547
Appendix
В
Problems
549
Appendix
С
References
568
Index
580 |
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| id | DE-604.BV035093667 |
| illustrated | Illustrated |
| index_date | 2024-07-02T22:11:31Z |
| indexdate | 2024-07-09T21:22:03Z |
| institution | BVB |
| isbn | 9780132224376 |
| language | English |
| lccn | 2008027095 |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-016761742 |
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| owner | DE-703 DE-634 DE-91G DE-BY-TUM DE-29T DE-706 |
| owner_facet | DE-703 DE-634 DE-91G DE-BY-TUM DE-29T DE-706 |
| physical | XVI, 590 S. Ill., graph. Darst. |
| publishDate | 2009 |
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| publishDateSort | 2009 |
| publisher | Prentice Hall |
| record_format | marc |
| spelling | Gas turbine theory H.I.H. Saravanamuttoo ... [et al.] 6. ed. Harlow, England ; Munich [u.a.] Prentice Hall 2009 XVI, 590 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier Includes bibliographical references and index Gas-turbines Gasturbine (DE-588)4019416-4 gnd rswk-swf Gasturbine (DE-588)4019416-4 s DE-604 Saravanamuttoo, H. I. Sonstige oth Bis 5. Auflage Saravanamuttoo, H. I. H. Gas turbine theory Digitalisierung UB Bayreuth application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=016761742&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Gas turbine theory 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 ... [et al.] |
| title_fullStr | Gas turbine theory H.I.H. Saravanamuttoo ... [et al.] |
| title_full_unstemmed | Gas turbine theory H.I.H. Saravanamuttoo ... [et al.] |
| title_old | Saravanamuttoo, H. I. H. Gas turbine theory |
| title_short | Gas turbine theory |
| title_sort | gas turbine theory |
| topic | Gas-turbines Gasturbine (DE-588)4019416-4 gnd |
| topic_facet | Gas-turbines Gasturbine |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=016761742&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
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