Cooling Of Gas Turbines 2
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Cooling Of Gas Turbines 2
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Author : Lincoln Wolfenstein
language : en
Publisher: BiblioGov
Release Date : 2013-07
Cooling Of Gas Turbines 2 written by Lincoln Wolfenstein and has been published by BiblioGov this book supported file pdf, txt, epub, kindle and other format this book has been release on 2013-07 with categories.
An analysis of rim cooling, which cools the blade by condition alone, was conducted. Gas temperatures ranged from 1300 degrees to 1900 degrees F and rim temperatures from 0 degrees to 1000 degrees F below gas temperatures. Results show that gas temperature increases up to 200 degrees F are permissible provided that the blades are cooled by 400 degrees to 500 degrees F below the gas temperature. Relatively small amounts of blade cooling, at constant gas temperature, give large increases in blade life. Dependence of rim cooling on heat-transfer coefficient, blade dimensions, and thermal conductivity is determined by a single parameter.
Cooling Of Gas Turbines Ii Effectiveness Of Rim Cooling Of Blades
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Author : Lincoln Wolfenstein
language : en
Publisher:
Release Date : 1947
Cooling Of Gas Turbines Ii Effectiveness Of Rim Cooling Of Blades written by Lincoln Wolfenstein and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1947 with categories.
Cooling Of Gas Turbines
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Author : W. Byron Brown
language : en
Publisher:
Release Date : 1947
Cooling Of Gas Turbines written by W. Byron Brown and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1947 with Aeronautics categories.
Cooling Of Gas Turbines
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Author : Lincoln Wolfenstein
language : en
Publisher:
Release Date : 1947
Cooling Of Gas Turbines written by Lincoln Wolfenstein and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1947 with Aeronautics categories.
Gas Turbine Heat Transfer And Cooling Technology Second Edition
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Author : Je-Chin Han
language : en
Publisher: CRC Press
Release Date : 2012-11-27
Gas Turbine Heat Transfer And Cooling Technology Second Edition written by Je-Chin Han and has been published by CRC Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2012-11-27 with Science categories.
A comprehensive reference for engineers and researchers, Gas Turbine Heat Transfer and Cooling Technology, Second Edition has been completely revised and updated to reflect advances in the field made during the past ten years. The second edition retains the format that made the first edition so popular and adds new information mainly based on selected published papers in the open literature. See What’s New in the Second Edition: State-of-the-art cooling technologies such as advanced turbine blade film cooling and internal cooling Modern experimental methods for gas turbine heat transfer and cooling research Advanced computational models for gas turbine heat transfer and cooling performance predictions Suggestions for future research in this critical technology The book discusses the need for turbine cooling, gas turbine heat-transfer problems, and cooling methodology and covers turbine rotor and stator heat-transfer issues, including endwall and blade tip regions under engine conditions, as well as under simulated engine conditions. It then examines turbine rotor and stator blade film cooling and discusses the unsteady high free-stream turbulence effect on simulated cascade airfoils. From here, the book explores impingement cooling, rib-turbulent cooling, pin-fin cooling, and compound and new cooling techniques. It also highlights the effect of rotation on rotor coolant passage heat transfer. Coverage of experimental methods includes heat-transfer and mass-transfer techniques, liquid crystal thermography, optical techniques, as well as flow and thermal measurement techniques. The book concludes with discussions of governing equations and turbulence models and their applications for predicting turbine blade heat transfer and film cooling, and turbine blade internal cooling.
Gas Turbines For Electric Power Generation
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Author : S. Can Gülen
language : en
Publisher: Cambridge University Press
Release Date : 2019-02-14
Gas Turbines For Electric Power Generation written by S. Can Gülen and has been published by Cambridge University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2019-02-14 with Science categories.
Everything you wanted to know about industrial gas turbines for electric power generation in one source with hard-to-find, hands-on technical information.
Cooling Of Gas Turbines
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Author : W. Byron Brown
language : en
Publisher:
Release Date : 1947
Cooling Of Gas Turbines written by W. Byron Brown and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1947 with Aeronautics categories.
Vaporization Cooling For Gas Turbines The Return Flow Cascade
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Author : Jack L. Kerrebrock
language : en
Publisher:
Release Date : 1998
Vaporization Cooling For Gas Turbines The Return Flow Cascade written by Jack L. Kerrebrock and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with categories.
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Stockholm, Sweden, June 2 - June 5, 1998.
Impingement Jet Cooling In Gas Turbines
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Author : R.S. Amano
language : en
Publisher: WIT Press
Release Date : 2014-05-28
Impingement Jet Cooling In Gas Turbines written by R.S. Amano and has been published by WIT Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 2014-05-28 with Science categories.
Due to the requirement for enhanced cooling technologies on modern gas turbine engines, advanced research and development has had to take place in field of thermal engineering. Among the gas turbine cooling technologies, impingement jet cooling is one of the most effective in terms of cooling effectiveness, manufacturability and cost. The chapters contained in this book describe research on state-of-the-art and advanced cooling technologies that have been developed, or that are being researched, with a variety of approaches from theoretical, experimental, and CFD studies. The authors of the chapters have been selected from some of the most active researchers and scientists on the subject. This is the first to book published on the topics of gas turbines and heat transfer to focus on impingement cooling alone.
Analysis And Comparison Of Wall Cooling Schemes For Advanced Gas Turbine Applications
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Author : Raymond Strong Colladay
language : en
Publisher:
Release Date : 1972
Analysis And Comparison Of Wall Cooling Schemes For Advanced Gas Turbine Applications written by Raymond Strong Colladay and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1972 with Cooling categories.
The relative performance of (1) counterflow film cooling, (2) parallel-flow film cooling, (3) convection cooling, (4) adiabatic film cooling, (5) transpiration cooling, and (6) full-coverage film cooling was investigated for heat loading conditions expected in future gas turbine engines. Assumed in the analysis were hot-gas conditions of 2200 K (3500 F) recovery temperature, 5 to 40 atmospheres total pressure, and 0.6 gas Mach number and a cooling air supply temperature of 811 K (1000 F). The first three cooling methods involve film cooling from slots. Counterflow and parallel flow describe the direction of convection cooling air along the inside surface of the wall relative to the main gas flow direction. The importance of utilizing the heat sink available in the coolant for convection cooling prior to film injection is illustrated.