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|n Title subscribed to via ProQuest Academic Complete
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050 |
0 |
0 |
|a TJ778
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|2 bisacsh
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|2 22
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|a UAMI
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|a Gas turbines: technology, efficiency, and performance /
|c Donna J. Ciafone, editor.
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264 |
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1 |
|a Hauppauge, New York :
|b Nova Science Publisher's,
|c [2011]
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300 |
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|a 1 online resource.
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336 |
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|a text
|b txt
|2 rdacontent
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337 |
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|a computer
|b c
|2 rdamedia
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338 |
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|a online resource
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347 |
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|a data file
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490 |
1 |
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|a Engineering tools, techniques and tables
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504 |
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|a Includes bibliographical references and index.
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588 |
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|a Description based on print version record.
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|a GAS TURBINES: TECHNOLOGY, EFFICIENCY AND PERFORMANCE ; GAS TURBINES: TECHNOLOGY, EFFICIENCY AND PERFORMANCE; CONTENTS ; PREFACE ; COMPREHENSIVE TECHNO-ECONOMIC EVALUATION OF GAS TURBINE REPOWERING SYSTEMS FOR UTILIZING WASTE HEAT FROM A SMALL SCALE REFUSE INCINERATION PLANT ; ABSTRACT ; 1. INTRODUCTION ; 2. OUTLINE OF INVESTIGATED SYSTEMS ; 2.1. Outline of a Refuse Incineration Plant and a Waste Heat Which Is Utilized ; 2.2. Outline of a System to Be Repowered ; 2.3. Outline of a Conventional Repowering System ; 2.4. Outline of the Proposed Repowering System (S-P1).
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505 |
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|a 2.5. Outline of the Proposed Repowering System (S-P2) 3. EVALUATION OF THERMODYNAMIC CHARACTERISTICS; 3.1. Premises ; 3.2. Estimated Characteristics of the STPS ; 3.3. Estimated Characteristics of The S-C ; 3.4. Estimated Characteristics of the S-P1 ; 3.5. Estimated Characteristics of the S-P2 ; 3.6. Discussions on the Estimated Thermodynamic Characteristics ; 3.7. Comparison of Thermodynamic Characteristics of the Rpss ; 4. EVALUATION OF ECONOMICS AND CO2-REDUCTION CHARACTERISTICS ; 4.1. Premises ; 4.2. Evaluation Results of the System to Be Repowered.
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505 |
8 |
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|a 4.3. Determination of the Best Operating Condition 4.4. Comparison of Economics and CO2 Reduction Characteristics of the Rpss ; 4.5. Discussions on Economical Effects of CO2-Capture of the S-P2 ; CONCLUSIONS; NOMENCLATURE ; ACKNOWLEDGMENTS ; REFERENCES ; IN-SERVICE DEGRADATION OF GAS TURBINE NOZZLES AND MOVING BLADES; ABSTRACT ; 1. INTRODUCTION ; 2. IN-SERVICE DEGRADATION OF THE FIRST STAGE NOZZLE OF A GAS TURBINE ; 2.1. Background ; 2.2. Microstructural Characterization of Nozzle Vane ; 2.3. Cracks Evaluating ; 2.4. Stress Evaluation ; 2.5. Discussion of Results ; 2.6. Conclusion.
|
505 |
8 |
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|a 3. IN-SERVICE DEGRADATION OF A GAS TURBINE MOVING BLADE MADE OF INCONEL 738LC ALLOY3.1. Background ; 3.2. Microstructural Characterization of a Gas Turbine Blade; Microstructural Evaluation of the Blade Root (Reference Zone) ; Microstructural Evaluation of Blade Hot Section (Airfoil) ; 3.3. Cracks Evaluating ; 3.4. Stress Evaluating ; 3.5 Discussion of Results ; 3.6. Conclusion ; FINAL CONCLUSION ; REFERENCES ; DESIGN AND DEVELOPMENT OF SMART COATINGS FOR TITANIUM ALLOYS USED IN GAS TURBINES ; ABSTRACT ; 1. INTRODUCTION ; 2. HIGH TEMPERATURE OXIDATION ; 3. LIFE PREDICTION MODELING.
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505 |
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|a 4. HOT CORROSION CHARACTERISTICS4.1. Degradation Mechanism ; 5. DEVELOPMENT OF HIGH PERFORMANCE COATINGS ; 6. DESIGN AND DEVELOPMENT OF SMART COATINGS ; SUMMARY ; REFERENCES ; THERMODYNAMIC OPTIMIZATION OF AN INTERCOOLED REHEAT REGENERATIVE GAS TURBINE POWER PLANT ; ABSTRACT ; INTRODUCTION; DESCRIPTION OF THE PROCESS ; THERMODYNAMIC MODELING ; Compressors Work ; Turbines Work ; Heat Input ; Work Output and Thermal Efficiency of the Plant ; Regenerator Criterion ; EFFICIENCY OPTIMIZATION ; FINAL NOTES ; CONCLUSION ; NOMENCLATURE ; REFERENCES.
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546 |
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|a English.
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590 |
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|a eBooks on EBSCOhost
|b EBSCO eBook Subscription Academic Collection - Worldwide
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650 |
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0 |
|a Gas-turbines.
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650 |
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6 |
|a Turbines à gaz.
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650 |
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7 |
|a gas turbines.
|2 aat
|
650 |
|
7 |
|a TECHNOLOGY & ENGINEERING
|x Mechanical.
|2 bisacsh
|
650 |
|
7 |
|a Gas-turbines
|2 fast
|
700 |
1 |
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|a Ciafone, Donna J.
|
776 |
0 |
8 |
|i Print version:
|t Gas turbines: technology, efficiency, and performance
|d Hauppauge, N.Y. : Nova Science Publisher's, c2011.
|z 9781611228427 (hardcover)
|w (DLC) 2010042613
|
830 |
|
0 |
|a Engineering tools, techniques and tables.
|
856 |
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