Experimental Data Correlations For The Effects Of Rotation On Impingement Cooling Of Turbine Blades
DOWNLOAD
Download Experimental Data Correlations For The Effects Of Rotation On Impingement Cooling Of Turbine Blades PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Experimental Data Correlations For The Effects Of Rotation On Impingement Cooling Of Turbine Blades book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page
Experimental Data Correlations For The Effects Of Rotation On Impingement Cooling Of Turbine Blades
DOWNLOAD
Author : J.C. Kreatsoulas
language : en
Publisher:
Release Date : 1987
Experimental Data Correlations For The Effects Of Rotation On Impingement Cooling Of Turbine Blades written by J.C. Kreatsoulas and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987 with categories.
Experimental Study Of Impingement Cooling In Rotating Turbine Blades
DOWNLOAD
Author : Massachusetts Institute of Technology. Gas Turbine & Plasma Dynamics Laboratory
language : en
Publisher:
Release Date : 1983
Experimental Study Of Impingement Cooling In Rotating Turbine Blades written by Massachusetts Institute of Technology. Gas Turbine & Plasma Dynamics Laboratory and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1983 with categories.
Gas Turbine Blade Cooling
DOWNLOAD
Author : Chaitanya D Ghodke
language : en
Publisher: SAE International
Release Date : 2018-12-10
Gas Turbine Blade Cooling written by Chaitanya D Ghodke and has been published by SAE International this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-12-10 with Technology & Engineering categories.
Gas turbines play an extremely important role in fulfilling a variety of power needs and are mainly used for power generation and propulsion applications. The performance and efficiency of gas turbine engines are to a large extent dependent on turbine rotor inlet temperatures: typically, the hotter the better. In gas turbines, the combustion temperature and the fuel efficiency are limited by the heat transfer properties of the turbine blades. However, in pushing the limits of hot gas temperatures while preventing the melting of blade components in high-pressure turbines, the use of effective cooling technologies is critical. Increasing the turbine inlet temperature also increases heat transferred to the turbine blade, and it is possible that the operating temperature could reach far above permissible metal temperature. In such cases, insufficient cooling of turbine blades results in excessive thermal stress on the blades causing premature blade failure. This may bring hazards to the engine's safe operation. Gas Turbine Blade Cooling, edited by Dr. Chaitanya D. Ghodke, offers 10 handpicked SAE International's technical papers, which identify key aspects of turbine blade cooling and help readers understand how this process can improve the performance of turbine hardware.
Impingement Jet Cooling In Gas Turbines
DOWNLOAD
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.
Nasa Technical Paper
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1984
Nasa Technical Paper written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1984 with Science categories.
International Aerospace Abstracts
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1998
International Aerospace Abstracts written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1998 with Aeronautics categories.
Rotational Effects On Impingement Cooling
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1985*
Rotational Effects On Impingement Cooling written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1985* with Gas-turbines categories.
Nasa Sp
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1993
Nasa Sp written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1993 with Aeronautics categories.
Effects Of Rotation On Coolant Passage Heat Transfer Volume 1 Coolant Passages With Smooth Walls
DOWNLOAD
Author : T. J. Hajek
language : en
Publisher:
Release Date : 1991
Effects Of Rotation On Coolant Passage Heat Transfer Volume 1 Coolant Passages With Smooth Walls written by T. J. Hajek and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1991 with categories.
Gas Turbine Heat Transfer And Cooling Technology Second Edition
DOWNLOAD
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.