Combustion instabilities in gas turbine engines [[electronic resource] ] : operational experience, fundamental mechanisms and modeling / / edited by Timothy C. Lieuwen, Vigor Yang |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2005 |
Descrizione fisica | 1 online resource (672 p.) |
Disciplina | 629.134/353 |
Altri autori (Persone) |
LieuwenTimothy C
YangVigor |
Collana | Progress in astronautics and aeronautics |
Soggetto topico | Gas-turbines - Combustion |
Soggetto genere / forma | Electronic books. |
ISBN |
1-60086-680-8
1-60086-461-9 1-61583-076-6 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Combustion instabilities: basic concepts -- Combustion instabilities in industrial gas turbines: Solar Turbine's experience -- Incorporation of combustion instability issues into design process: GE aeroderivative and aero engines experience -- Combustion instability and its passive control: Rolls-Royce aeroderivative engine experience -- Thermoacoustic design tools and passive control: Siemens power generation approaches -- Characterization and control of aeroengine combustion Instability: Pratt & Whitney and NASA experience -- Monitoring of combustion instabilities: Calpine's experience -- Monitoring combustion instabilities: E.ON UK's experience -- Combustion instability mechanisms in premixed combustors -- Flow and flame dynamics of lean premixed swirl Injectors -- Acoustic-vortex-flame interactions in gas turbines -- Physics of premixed combustion-acoustic wave interactions -- Acoustic analysis of gas-turbine combustors -- Three-dimensional linear stability analysis of gas turbine combustion dynamics -- Implementation of instability prediction in design: ALSTOM approaches -- Experimental diagnostics of combustion instabilities -- Passive control of combustion instabilities in stationary gas turbines -- Factors affecting the control of unstable combustors -- Implementation of active control in a full-scale gas-turbine combustor. |
Record Nr. | UNINA-9910454437903321 |
Reston, Va., : American Institute of Aeronautics and Astronautics, c2005 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Combustion instabilities in gas turbine engines [[electronic resource] ] : operational experience, fundamental mechanisms and modeling / / edited by Timothy C. Lieuwen, Vigor Yang |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2005 |
Descrizione fisica | 1 online resource (672 p.) |
Disciplina | 629.134/353 |
Altri autori (Persone) |
LieuwenTimothy C
YangVigor |
Collana | Progress in astronautics and aeronautics |
Soggetto topico | Gas-turbines - Combustion |
ISBN |
1-60086-680-8
1-60086-461-9 1-61583-076-6 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Combustion instabilities: basic concepts -- Combustion instabilities in industrial gas turbines: Solar Turbine's experience -- Incorporation of combustion instability issues into design process: GE aeroderivative and aero engines experience -- Combustion instability and its passive control: Rolls-Royce aeroderivative engine experience -- Thermoacoustic design tools and passive control: Siemens power generation approaches -- Characterization and control of aeroengine combustion Instability: Pratt & Whitney and NASA experience -- Monitoring of combustion instabilities: Calpine's experience -- Monitoring combustion instabilities: E.ON UK's experience -- Combustion instability mechanisms in premixed combustors -- Flow and flame dynamics of lean premixed swirl Injectors -- Acoustic-vortex-flame interactions in gas turbines -- Physics of premixed combustion-acoustic wave interactions -- Acoustic analysis of gas-turbine combustors -- Three-dimensional linear stability analysis of gas turbine combustion dynamics -- Implementation of instability prediction in design: ALSTOM approaches -- Experimental diagnostics of combustion instabilities -- Passive control of combustion instabilities in stationary gas turbines -- Factors affecting the control of unstable combustors -- Implementation of active control in a full-scale gas-turbine combustor. |
Record Nr. | UNINA-9910782756303321 |
Reston, Va., : American Institute of Aeronautics and Astronautics, c2005 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Combustion instabilities in gas turbine engines [[electronic resource] ] : operational experience, fundamental mechanisms and modeling / / edited by Timothy C. Lieuwen, Vigor Yang |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2005 |
Descrizione fisica | 1 online resource (672 p.) |
Disciplina | 629.134/353 |
Altri autori (Persone) |
LieuwenTimothy C
YangVigor |
Collana | Progress in astronautics and aeronautics |
Soggetto topico | Gas-turbines - Combustion |
ISBN |
1-60086-680-8
1-60086-461-9 1-61583-076-6 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Combustion instabilities: basic concepts -- Combustion instabilities in industrial gas turbines: Solar Turbine's experience -- Incorporation of combustion instability issues into design process: GE aeroderivative and aero engines experience -- Combustion instability and its passive control: Rolls-Royce aeroderivative engine experience -- Thermoacoustic design tools and passive control: Siemens power generation approaches -- Characterization and control of aeroengine combustion Instability: Pratt & Whitney and NASA experience -- Monitoring of combustion instabilities: Calpine's experience -- Monitoring combustion instabilities: E.ON UK's experience -- Combustion instability mechanisms in premixed combustors -- Flow and flame dynamics of lean premixed swirl Injectors -- Acoustic-vortex-flame interactions in gas turbines -- Physics of premixed combustion-acoustic wave interactions -- Acoustic analysis of gas-turbine combustors -- Three-dimensional linear stability analysis of gas turbine combustion dynamics -- Implementation of instability prediction in design: ALSTOM approaches -- Experimental diagnostics of combustion instabilities -- Passive control of combustion instabilities in stationary gas turbines -- Factors affecting the control of unstable combustors -- Implementation of active control in a full-scale gas-turbine combustor. |
Record Nr. | UNINA-9910824692903321 |
Reston, Va., : American Institute of Aeronautics and Astronautics, c2005 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Combustion instabilities in liquid rocket engines [[electronic resource] ] : testing and development practices in Russia / / Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley |
Autore | Dranovsky Mark L |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 |
Descrizione fisica | 1 online resource (342 p.) |
Disciplina | 621.43/56 |
Altri autori (Persone) |
YangVigor
CulickF <1933-> (Fred) TalleyDouglas G |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Liquid propellant rockets
Rocket engines - Combustion - Russia (Federation) - Testing Liquid fuels - Combustion - Russia (Federation) - Testing Rockets (Aeronautics) - Russia (Federation) - Testing |
Soggetto genere / forma | Electronic books. |
ISBN |
1-60086-690-5
1-60086-471-6 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Introduction -- Terms and definitions -- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level -- Uncertainty in conversion of propellant to combustion products -- Studies of operating process stability at various stages of combustor development -- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators -- Acoustic study of combustion chamber stability characteristics -- Determination of stability of oscillations from natural disturbances -- Evaluation of LRE process stability by use of artificial pressure disturbances -- Model firing tests for selection of injector head elements -- Estimation of operating process stability from pressure oscillation decrements -- Test results for pulsing liquid-liquid chambers -- Stability of gas-liquid combustion chambers -- Gas-liquid combustion-chamber tests for stability to hard excitation -- Injector head for RD-170 engine combustion chamber -- Stability characteristics of engines with adjustable injectors -- Control of stability in production of the proton engine. |
Record Nr. | UNINA-9910457203903321 |
Dranovsky Mark L | ||
Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Combustion instabilities in liquid rocket engines [[electronic resource] ] : testing and development practices in Russia / / Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley |
Autore | Dranovsky Mark L |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 |
Descrizione fisica | 1 online resource (342 p.) |
Disciplina | 621.43/56 |
Altri autori (Persone) |
YangVigor
CulickF <1933-> (Fred) TalleyDouglas G |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Liquid propellant rockets
Rocket engines - Combustion - Russia (Federation) - Testing Liquid fuels - Combustion - Russia (Federation) - Testing Rockets (Aeronautics) - Russia (Federation) - Testing |
ISBN |
1-60086-690-5
1-60086-471-6 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Introduction -- Terms and definitions -- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level -- Uncertainty in conversion of propellant to combustion products -- Studies of operating process stability at various stages of combustor development -- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators -- Acoustic study of combustion chamber stability characteristics -- Determination of stability of oscillations from natural disturbances -- Evaluation of LRE process stability by use of artificial pressure disturbances -- Model firing tests for selection of injector head elements -- Estimation of operating process stability from pressure oscillation decrements -- Test results for pulsing liquid-liquid chambers -- Stability of gas-liquid combustion chambers -- Gas-liquid combustion-chamber tests for stability to hard excitation -- Injector head for RD-170 engine combustion chamber -- Stability characteristics of engines with adjustable injectors -- Control of stability in production of the proton engine. |
Record Nr. | UNINA-9910781700303321 |
Dranovsky Mark L | ||
Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Combustion instabilities in liquid rocket engines [[electronic resource] ] : testing and development practices in Russia / / Mark L. Dranovsky ; edited by Vigor Yang, Fred E.C. Culick, Douglas G. Talley |
Autore | Dranovsky Mark L |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 |
Descrizione fisica | 1 online resource (342 p.) |
Disciplina | 621.43/56 |
Altri autori (Persone) |
YangVigor
CulickF <1933-> (Fred) TalleyDouglas G |
Collana | Progress in astronautics and aeronautics |
Soggetto topico |
Liquid propellant rockets
Rocket engines - Combustion - Russia (Federation) - Testing Liquid fuels - Combustion - Russia (Federation) - Testing Rockets (Aeronautics) - Russia (Federation) - Testing |
ISBN |
1-60086-690-5
1-60086-471-6 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Introduction -- Terms and definitions -- Mechanisms of transition from noise to high-frequency oscillations or to noise at a new level -- Uncertainty in conversion of propellant to combustion products -- Studies of operating process stability at various stages of combustor development -- Quantitative characteristics for estimating stability of LRE combustion chambers for gas generators -- Acoustic study of combustion chamber stability characteristics -- Determination of stability of oscillations from natural disturbances -- Evaluation of LRE process stability by use of artificial pressure disturbances -- Model firing tests for selection of injector head elements -- Estimation of operating process stability from pressure oscillation decrements -- Test results for pulsing liquid-liquid chambers -- Stability of gas-liquid combustion chambers -- Gas-liquid combustion-chamber tests for stability to hard excitation -- Injector head for RD-170 engine combustion chamber -- Stability characteristics of engines with adjustable injectors -- Control of stability in production of the proton engine. |
Record Nr. | UNINA-9910817251603321 |
Dranovsky Mark L | ||
Reston, Va., : American Institute of Aeronautics and Astronautics, c2007 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Gas turbine emissions / / edited by Tim C. Lieuwen, Georgia Institute of Technology, Vigor Yang, Georgia Institute of Technology [[electronic resource]] |
Autore | Lieuwen Timothy C. |
Pubbl/distr/stampa | Cambridge : , : Cambridge University Press, , 2013 |
Descrizione fisica | 1 online resource (xvi, 368 pages) : digital, PDF file(s) |
Disciplina | 621.43/3 |
Collana | Cambridge aerospace series |
Soggetto topico |
Gas-turbines - Environmental aspects
Gas-turbines - Combustion Combustion gases - Environmental aspects |
ISBN |
1-316-09062-0
1-299-74898-8 1-107-24978-3 1-107-24812-4 1-62870-281-8 1-107-24895-7 1-107-25061-7 1-107-24729-2 1-139-01546-X |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Forward / Alan H. Epstein -- Preface / Timothy C. Lieuwen, Vigor Yang -- Section 1. Overview and Key Issues -- Aero GT Combustion : Metrics, Constraints and System Interactions / Lead: Randy McKinney, Pratt & Whitney -- Ground based GT combustion : Metrics, Constraints and System Interactions / Lead: Vince McDonell, University of California, Irvine -- Overview of Worldwide Aircraft Regulatory Framework / Lead: Will Dodds, GE Aircraft Engines, williard.dodd@ge.com -- Overview of Worldwide Ground-Based Regulatory Framework / Lead: Manfred Klein, Canadian National Research Council -- Section 2. Fundamentals and Modeling : Production and Control -- Particulate Formation / Lead: Med Colket, United Technologies Research Center -- Gaseous Aerosol Precursors / Lead: Rick Miake-Lye, Aerodyne -- NOx and CO Formation and Control / Lead: Mike Klassen -- Emissions from Oxyfueled or High Exhaust Gas Recirculation Turbines / Lead: Jerry M. Seitzman -- Section 3. Case Studies and Specific Technologies : Pollutant Trends and Key Drivers -- Partially Premixed, and Premixed Aeroengine Combustors / Lead: Christoph Hassa, DLR -- Industrial Combustors : Conventional, non-premixed and Dry Low Emissions (DLN) / Lead: Thomas Sattelmayer, TU Munchen. |
Record Nr. | UNINA-9910464928103321 |
Lieuwen Timothy C. | ||
Cambridge : , : Cambridge University Press, , 2013 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Gas turbine emissions / / edited by Tim C. Lieuwen, Georgia Institute of Technology, Vigor Yang, Georgia Institute of Technology [[electronic resource]] |
Autore | Lieuwen Timothy C. |
Pubbl/distr/stampa | Cambridge : , : Cambridge University Press, , 2013 |
Descrizione fisica | 1 online resource (xvi, 368 pages) : digital, PDF file(s) |
Disciplina | 621.43/3 |
Collana | Cambridge aerospace series |
Soggetto topico |
Gas-turbines - Environmental aspects
Gas-turbines - Combustion Combustion gases - Environmental aspects |
ISBN |
1-316-09062-0
1-299-74898-8 1-107-24978-3 1-107-24812-4 1-62870-281-8 1-107-24895-7 1-107-25061-7 1-107-24729-2 1-139-01546-X |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Forward / Alan H. Epstein -- Preface / Timothy C. Lieuwen, Vigor Yang -- Section 1. Overview and Key Issues -- Aero GT Combustion : Metrics, Constraints and System Interactions / Lead: Randy McKinney, Pratt & Whitney -- Ground based GT combustion : Metrics, Constraints and System Interactions / Lead: Vince McDonell, University of California, Irvine -- Overview of Worldwide Aircraft Regulatory Framework / Lead: Will Dodds, GE Aircraft Engines, williard.dodd@ge.com -- Overview of Worldwide Ground-Based Regulatory Framework / Lead: Manfred Klein, Canadian National Research Council -- Section 2. Fundamentals and Modeling : Production and Control -- Particulate Formation / Lead: Med Colket, United Technologies Research Center -- Gaseous Aerosol Precursors / Lead: Rick Miake-Lye, Aerodyne -- NOx and CO Formation and Control / Lead: Mike Klassen -- Emissions from Oxyfueled or High Exhaust Gas Recirculation Turbines / Lead: Jerry M. Seitzman -- Section 3. Case Studies and Specific Technologies : Pollutant Trends and Key Drivers -- Partially Premixed, and Premixed Aeroengine Combustors / Lead: Christoph Hassa, DLR -- Industrial Combustors : Conventional, non-premixed and Dry Low Emissions (DLN) / Lead: Thomas Sattelmayer, TU Munchen. |
Record Nr. | UNINA-9910789314303321 |
Lieuwen Timothy C. | ||
Cambridge : , : Cambridge University Press, , 2013 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Gas turbine emissions / / edited by Tim C. Lieuwen, Georgia Institute of Technology, Vigor Yang, Georgia Institute of Technology [[electronic resource]] |
Autore | Lieuwen Timothy C. |
Pubbl/distr/stampa | Cambridge : , : Cambridge University Press, , 2013 |
Descrizione fisica | 1 online resource (xvi, 368 pages) : digital, PDF file(s) |
Disciplina | 621.43/3 |
Collana | Cambridge aerospace series |
Soggetto topico |
Gas-turbines - Environmental aspects
Gas-turbines - Combustion Combustion gases - Environmental aspects |
ISBN |
1-316-09062-0
1-299-74898-8 1-107-24978-3 1-107-24812-4 1-62870-281-8 1-107-24895-7 1-107-25061-7 1-107-24729-2 1-139-01546-X |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto | Forward / Alan H. Epstein -- Preface / Timothy C. Lieuwen, Vigor Yang -- Section 1. Overview and Key Issues -- Aero GT Combustion : Metrics, Constraints and System Interactions / Lead: Randy McKinney, Pratt & Whitney -- Ground based GT combustion : Metrics, Constraints and System Interactions / Lead: Vince McDonell, University of California, Irvine -- Overview of Worldwide Aircraft Regulatory Framework / Lead: Will Dodds, GE Aircraft Engines, williard.dodd@ge.com -- Overview of Worldwide Ground-Based Regulatory Framework / Lead: Manfred Klein, Canadian National Research Council -- Section 2. Fundamentals and Modeling : Production and Control -- Particulate Formation / Lead: Med Colket, United Technologies Research Center -- Gaseous Aerosol Precursors / Lead: Rick Miake-Lye, Aerodyne -- NOx and CO Formation and Control / Lead: Mike Klassen -- Emissions from Oxyfueled or High Exhaust Gas Recirculation Turbines / Lead: Jerry M. Seitzman -- Section 3. Case Studies and Specific Technologies : Pollutant Trends and Key Drivers -- Partially Premixed, and Premixed Aeroengine Combustors / Lead: Christoph Hassa, DLR -- Industrial Combustors : Conventional, non-premixed and Dry Low Emissions (DLN) / Lead: Thomas Sattelmayer, TU Munchen. |
Record Nr. | UNINA-9910822227703321 |
Lieuwen Timothy C. | ||
Cambridge : , : Cambridge University Press, , 2013 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|
Liquid rocket thrust chambers [[electronic resource] ] : aspects of modeling, analysis, and design / / edited by Vigor Yang ... [et al.] |
Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2004 |
Descrizione fisica | 1 online resource (760 p.) |
Disciplina | 662.6/66 |
Altri autori (Persone) | YangVigor |
Collana | Progress in astronautics and aeronautics |
Soggetto topico | Liquid propellants |
Soggetto genere / forma | Electronic books. |
ISBN |
1-60086-676-X
1-60086-457-0 1-61583-080-4 |
Formato | Materiale a stampa |
Livello bibliografico | Monografia |
Lingua di pubblicazione | eng |
Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Acknowledgments""; ""Chapter 1 Propellant Injection Systems and Processes""; ""Introduction""; ""Rocket Application Design Requirements""; ""Thrust Level and Operating Pressure""; ""Propellant Type""; ""Engine Cycle or Feed System""; ""Common Combustion Device Development Risks""; ""Combustion Instability""; ""Combustion Chamber Overheating and Burnout""; ""Injector Face Erosion""; ""Low Thrust Chamber Assembly Performance""; ""Unsafe Transients""; ""Injection System Design Considerations""
""Engine Pressure Schedule""""Nozzle Expansion Ratio""; ""Contraction Ratio""; ""Chamber Length""; ""Injection Element and Pattern""; ""Critical Combustion Processes""; ""Injector Manifold Distribution""; ""Injector Spray Atomization""; ""Propellant Droplet Vaporization""; ""Bipropellant Mixing""; ""Candidate Injectors for Liquid Rocket Applications""; ""Coaxial Jet Injectors""; ""Impinging Jet Injectors""; ""Parallel Jet (Showerhead) Injectors""; ""Injector Design Synthesis""; ""Conclusions and R e commendations""; ""References""; ""Chapter 2 Design and Dynamics of Jet and Swirl Injectors"" ""Nomenclature""""Introduction""; ""Classification of Injectors and Methods of Mixture Formation""; ""Liquid Injectors""; ""Gas-Liquid Injectors""; ""Intensification of Propellant Atomization and Mixing in Liquid Injectors""; ""Intensification of Propellant Atomization and Mixing in Gas-Liquid Injectors""; ""Theory and Design of Liquid Monopropellant Jet Injectors""; ""Flow Characteristics""; ""Effect of Injector Configuration""; ""Flow Coefficient""; ""Design Procedure""; ""Theory and Design of Gaseous Monopropellant Jet Injectors""; ""Flow Characteristics""; ""Design Procedure"" ""Theory and Design of Gas-Liquid Jet Injectors""""Theory and Design of Liquid Monopropellant Swirl Injectors""; ""Flow Characteristics of Ideal Swirl Injector""; ""Flow Characteristics of Real Swirl Injectors""; ""Effect of Viscosity on Injector Operation""; ""Design Procedure""; ""Theory and Design of Liquid Bipropellant Swirl Injectors""; ""Injectors with External Mixing""; ""Injectors with Internal Mixing""; ""Modulation of Liquid Spray Characteristics of Swirl Injectors""; ""Design of Gas Swirl Injectors""; ""Design Procedure""; ""Selection of Geometric Dimensions and Flow Parameters"" ""Dynamics of Liquid Rocket Injectors""""Linear Dynamics of Jet Injectors""; ""Linear Dynamics of Swirl Injectors""; ""Acknowledgments""; ""References""; ""Chapter 3 Atomization in Coaxial-Jet Injectors""; ""Nomenclature""; ""Introduction""; ""Phenomenological Description and Literature Review""; ""General Scheme of Jet Disintegration and Drop Formation""; ""Studies of Elementary Processes""; ""Numerical Simulations of the Atomization Process""; ""Derivation of Droplet Size Distribution Functions""; ""Investigations of Atomization in Shear Coaxial Injectors"" ""Experimental and Theoretical Investigation at Atmospheric Pressure with Simulants"" |
Record Nr. | UNINA-9910455264103321 |
Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., c2004 | ||
Materiale a stampa | ||
Lo trovi qui: Univ. Federico II | ||
|