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Gas turbine theory:

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Bibliographische Detailangaben
Beteiligte Personen:	Cohen, Henry (VerfasserIn), Rogers, Gordon F. C. 1921- (VerfasserIn), Saravanamuttoo, H. I. (VerfasserIn)
Format:	Buch
Sprache:	Nichtbestimmte Sprache
Veröffentlicht:	Harlow, Essex, England u.a. Longman u.a. 1987
Ausgabe:	3. ed.
Schlagwörter:	Gasturbine
Links:	http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=001347559&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA
Umfang:	XII, 414 S. Ill., graph. Darst.
ISBN:	058230539X

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Datensatz im Suchindex

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adam_text	THIRD EDITION GAS TURBINE THEORY H. COHEN FELLOW, QUEENS COLLEGE, UNIVERSITY OF CAMBRIDGE G. F. C. ROGERS PROFESSOR EMERITUS, UNIVERSITY OF BRISTOL H. I. H. SARAVANAMUTTOO PROFESSOR, DEPARTMENT OF MECHANICAL AND AERONAUTICAL ENGINEERING, CARLETON UNIVERSITY PI PI PI PI PI PI LONGMAN SCIENTIFIC & TECHNICAL COPUBLISHED IN THE. UNITED STATES WITH JOHN WILEY & SONS, INC., NEW YORK CONTENTS PREFACES IX 1 INTRODUCTION 1 1.1 OPEN CYCLE SINGLE-SHAFT AND TWIN-SHAFT ARRANGEMENTS 5 1.2 MULTI-SPOOL ARRANGEMENTS 7 1.3 CLOSED CYCLES 9 1.4 AIRCRAFT PROPULSION 10 1.5 INDUSTRIAL APPLICATIONS 17 1.6 SOME FUTURE POSSIBILITIES 25 1.7 GAS TURBINE DESIGN PROCEDURE 28 SHAFT POWER CYCLES 32 2.1 IDEAL CYCLES 32 2.2 METHODS OF ACCOUNTING FOR COMPONENT LOSSES 40 2.3 DESIGN POINT PERFORMANCE CALCULATIONS 56 2.4 COMPARATIVE PERFORMANCE OF PRACTICAL CYCLES 61 2.5 COGAS CYCLES AND COGENERATION SCHEMES 67 2.6 CLOSED CYCLE GAS TURBINES 70 GAS TURBINE CYCLES FOR AIRCRAFT PROPULSION 76 3.1 CRITERIA OF PERFORMANCE 76 3.2 INTAKE AND PROPELLING NOZZLE EFFICIENCIES 80 3.3 SIMPLE TURBOJET CYCLE 87 3.4 THE TURBOFAN ENGINE 93 3.5 THE TURBOPROP ENGINE 102 3.6 THRUST AUGMENTATION 105 4 CENTRIFUGAL COMPRESSORS 109 4.1 PRINCIPLE OF OPERATION 110 CONTENTS 4.2 WORK DONE AND PRESSURE RISE 111 4.3 THE DIFFUSER . 119 4.4 COMPRESSIBILITY EFFECTS 125 4.5 NON-DIMENSIONAL QUANTITIES FOR PLOTTING COMPRESSOR CHARACTERISTICS 130 4.6 COMPRESSOR CHARACTERISTICS 132 4.7 COMPUTERISED DESIGN PROCEDURES 136 AXIAL FLOW COMPRESSORS 138 5.1 BASIC OPERATION 139 5.2 ELEMENTARY THEORY 141 5.3 FACTORS AFFECTING STAGE PRESSURE RATIO 144 5.4 BLOCKAGE IN THE COMPRESSOR ANNULUS 150 5.5 DEGREE OF REACTION 152 5.6 THREE-DIMENSIONAL FLOW 154 5.7 DESIGN PROCESS 164 5.8 BLADE DESIGN 185 5.9 CALCULATION OF STAGE PERFORMANCE 195 5.10 COMPRESSIBILITY EFFECTS 204 5.11 OFF-DESIGN PERFORMANCE 210 5.12 AXIAL COMPRESSOR CHARACTERISTICS 213 5.13 CLOSURE 219 COMBUSTION SYSTEMS 221 6.1 FORM OF COMBUSTION SYSTEM 221 6.2 SOME IMPORTANT FACTORS AFFECTING COMBUSTION CHAMBER DESIGN 223 6.3 THE COMBUSTION PROCESS 225 6.4 COMBUSTION CHAMBER PERFORMANCE 229 6.5 SOME PRACTICAL PROBLEMS 236 AXIAL AND RADICAL FLOW TURBINES 244 7.1 ELEMENTARY THEORY OF AXIAL FLOW TURBINE 244 7.2 VORTEX THEORY 261 7.3 CHOICE OF BLADE PROFILE, PITCH AND CHORD 267 7.4 ESTIMATION OF STAGE PERFORMANCE 283 7.5 OVERALL TURBINE PERFORMANCE 292 7.6 THE COOLED TURBINE 294 7.7 THE RADIAL FLOW TURBINE 301 8 PREDICTION OF PERFORMANCE OF SIMPLE GAS TURBINES 309 8.1 COMPONENT CHARACTERISTICS 311 ENTS VU 8.2 OFF-DESIGN OPERATION OF THE SINGLE-SHAFT GAS TURBINE 313 8.3 EQUILIBRIUM RUNNING OF A GAS GENERATOR 318 8.4 OFF-DESIGN OPERATION OF FREE TURBINE ENGINE 321 8.5 OFF-DESIGN OPERATION OF THE JET ENGINE 330 8.6 METHODS OF DISPLACING THE EQUILIBRIUM RUNNING LINE 338 8.7 INCORPORATION OF VARIABLE PRESSURE LOSSES 342 PREDICTION OF PERFORMANCE*FURTHER TOPICS 344 9.1 METHODS OF IMPROVING PART-LOAD PERFORMANCE 344 9.2 MATCHING PROCEDURES FOR TWIN-SPOOL ENGINES 349 9.3 SOME NOTES ON THE BEHAVIOUR OF TWIN-SPOOL ENGINES 353 9.4 MATCHING PROCEDURES FOR TURBOFAN ENGINES 357 9.5 TRANSIENT BEHAVIOUR OF GAS TURBINES 359 9.6 PRINCIPLES OF CONTROL SYSTEMS 366 APPENDIX A SOME NOTES ON GAS DYNAMICS 370 A.I COMPRESSIBILITY EFFECTS (QUALITATIVE TREATMENT) 370 A.2 BASIC EQUATIONS FOR STEADY ONE-DIMENSIONAL COMPRESSIBLE FLOW OF A PERFECT GAS IN A DUCT 374 A.3 ISENTROPIC FLOW IN A DUCT OF VARYING AREA 376 A.4 FRICTIONLESS FLOW IN A CONSTANT AREA DUCT WITH HEAT TRANSFER 377 A.5 ADIABATIC FLOW IN A CONSTANT AREA DUCT WITH FRICTION 379 A.6 PLANE NORMAL SHOCK WAVES 380 A.7 OBLIQUE SHOCK WAVES 384 A.8 ISENTROPIC TWO-DIMENSIONAL SUPERSONIC EXPANSION AND COMPRESSION 387 APPENDIX B PROBLEMS 390 APPENDIX C REFERENCES 402 INDEX 407
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author	Cohen, Henry Rogers, Gordon F. C. 1921- Saravanamuttoo, H. I.
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indexdate	2024-12-20T07:45:27Z
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isbn	058230539X
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physical	XII, 414 S. Ill., graph. Darst.
publishDate	1987
publishDateSearch	1987
publishDateSort	1987
publisher	Longman u.a.
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spellingShingle	Cohen, Henry Rogers, Gordon F. C. 1921- Saravanamuttoo, H. I. Gas turbine theory 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. Cohen ; G. F. C. Rogers ; H. I. H. Saravanamuttoo
title_fullStr	Gas turbine theory H. Cohen ; G. F. C. Rogers ; H. I. H. Saravanamuttoo
title_full_unstemmed	Gas turbine theory H. Cohen ; G. F. C. Rogers ; H. I. H. Saravanamuttoo
title_short	Gas turbine theory
title_sort	gas turbine theory
topic	Gasturbine (DE-588)4019416-4 gnd
topic_facet	Gasturbine
url	http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=001347559&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA
work_keys_str_mv	AT cohenhenry gasturbinetheory AT rogersgordonfc gasturbinetheory AT saravanamuttoohi gasturbinetheory

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