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Basic Aspects of Gas Turbine Heat Transfer

2017 Technology
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Release : 2017
Genre : Technology
Kind : eBook
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Book Synopsis Basic Aspects of Gas Turbine Heat Transfer by : Shailendra Naik

Download or read book Basic Aspects of Gas Turbine Heat Transfer written by Shailendra Naik. This book was released on 2017. Available in PDF, EPUB and Kindle. Book excerpt: The use of gas turbines for power generation and electricity production in both single cycle and combined cycle plant operation is extensive and will continue to globally grow into the future. Due to its high power density and ability to convert gaseous and liquid fuel into mechanical work with very high thermodynamic efficiencies, significant efforts continue today to further increase both the power output and thermodynamic efficiencies of the gas turbine. In particular, the aerothermal design of gas turbine components has progressed at a rapid pace in the last decade with all gas turbine manufacturers, in order to achieve higher thermodynamic efficiencies. This has been achieved by using higher turbine inlet temperatures and pressures, advanced turbine aerodynamics and efficient cooling systems of turbine airofoils, and advanced high temperature alloys, metallic coatings, and ceramic thermal barrier coatings. In this chapter, issues related to the thermal design of gas turbine blades are highlighted and several heat transfer technologies are examined, such as convective cooling, impingement cooling, film cooling, and application of thermal barrier coatings. Typical methods for validating the thermal designs of gas turbine airofoils are also outlined.

Gas Turbine Heat Transfer and Cooling Technology

2012-11-27 Science
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Release : 2012-11-27
Genre : Science
Kind : eBook
Book Rating : 903/5 ( reviews)

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Book Synopsis Gas Turbine Heat Transfer and Cooling Technology by : Je-Chin Han

Download or read book Gas Turbine Heat Transfer and Cooling Technology written by Je-Chin Han. This book was released on 2012-11-27. Available in PDF, EPUB and Kindle. Book excerpt: A comprehensive reference for engineers and researchers, this second edition focuses on gas turbine heat transfer issues and their associated cooling technologies for aircraft and land-based gas turbines. It provides information on state-of-the-art cooling technologies such as advanced turbine blade film cooling and internal cooling schemes. The book also offers updated experimental methods for gas turbine heat transfer and cooling research, as well as advanced computational models for gas turbine heat transfer and cooling performance predictions. The authors provide suggestions for future research within this technology and includes 800 illustrations to help clarify concepts and instruction.

Fundamental Heat Transfer Research for Gas Turbine Engines

1980 Gas-turbine industry
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Release : 1980
Genre : Gas-turbine industry
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Book Synopsis Fundamental Heat Transfer Research for Gas Turbine Engines by :

Download or read book Fundamental Heat Transfer Research for Gas Turbine Engines written by . This book was released on 1980. Available in PDF, EPUB and Kindle. Book excerpt:

Heat Transfer in Gas Turbines

2001 Medical
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Release : 2001
Genre : Medical
Kind : eBook
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Book Synopsis Heat Transfer in Gas Turbines by : Bengt Sundén

Download or read book Heat Transfer in Gas Turbines written by Bengt Sundén. This book was released on 2001. Available in PDF, EPUB and Kindle. Book excerpt: This title presents and reflects current active research on various heat transfer topics and related phenomena in gas turbine systems. It begins with a general introduction to gas turbine heat transfer, before moving on to specific areas.

Combustion and Heat Transfer in Gas Turbine Systems

2013-10-22 Technology & Engineering
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Release : 2013-10-22
Genre : Technology & Engineering
Kind : eBook
Book Rating : 794/5 ( reviews)

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Book Synopsis Combustion and Heat Transfer in Gas Turbine Systems by : E. R. Norster

Download or read book Combustion and Heat Transfer in Gas Turbine Systems written by E. R. Norster. This book was released on 2013-10-22. Available in PDF, EPUB and Kindle. Book excerpt: Combustion and Heat Transfer in Gas Turbine Systems is a compilation of papers from the Proceedings of an International Propulsion Symposium held at the College of Aeronautics, Cranfield in April 1969. This compilation deals with research done by academic and scientific institutions and of industrial organizations, with some research papers covering atomization, fuels, and high-temperature materials. One paper describes the combustion system of the Concorde engine used in commercial flights, temperature of metal parts, and some design modifications to increase the mechanical life of the combustion system. Another paper discusses the evolution of the RB 162 combustion system that is used in the vertical takeoff and landing aircrafts. The RB 162 has many design features of the earlier single reversal chamber and differs in only one or two points. The book then notes the necessity of a plenum chamber burning to further development of supersonic engines and flight. One paper also proposes an alternative theory to the traditional ignition theory of altitude relighting such as those developed by Lewis and von Elbe. Another paper reposts on some observations made of the atomizing characteristics of air-blast atomizers and proposes simple changes to improve the performance of the atomizer by prefilming and allowing air to both sides of the fuel. This compilation will prove very helpful for aeronautical engineers, aviation designers, physicists, students of engineering, and readers who are interested in the design and development of jet engines and supersonic aircrafts.

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