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New Title:	Gas turbine theory
Main Authors:	Saravanamuttoo, H. I. (Author), Rogers, Gordon F. C. 1921- (Author), Cohen, Henry (Author)
Format:	Book
Language:	English
Published:	Harlow ; Munich [u.a.] Prentice Hall 2001
Edition:	5. ed.
Subjects:	Gasmotoren Turbinas a gás Turbines Gas-turbines Gasturbine
Links:	http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=009672641&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA
Item Description:	Bis 4. ed. u.d.T.: Cohen, Henry : Gas turbine theory
Physical Description:	XVI, 491 S. Ill., graph. Darst.
ISBN:	013015847X

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Record in the Search Index

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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
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spellingShingle	Saravanamuttoo, H. I. Rogers, Gordon F. C. 1921- 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_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_new	Gas turbine theory
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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work_keys_str_mv	AT saravanamuttoohi gasturbinetheory AT rogersgordonfc gasturbinetheory AT cohenhenry gasturbinetheory

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Call Number:	0702 MAS 585f 07.2002 A 334 Floor plan
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