Author: A. Kaufman
Publisher:
ISBN:
Category : Gliders (Aeronautics)
Languages : en
Pages : 36
Book Description
Analytical Study of Cooled Turbine Blades Considering Combined Steady-state and Transient Conditions
Author: A. Kaufman
Publisher:
ISBN:
Category : Gliders (Aeronautics)
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Gliders (Aeronautics)
Languages : en
Pages : 36
Book Description
An Analysis of the Capabilities and Limitations of Turbine Air Cooling Methods
Author: Jack B. Esgar
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 60
Book Description
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 60
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892
Book Description
U.S. Government Research & Development Reports
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 238
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 238
Book Description
NASA Technical Memorandum
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 384
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 384
Book Description
Gas Turbine Blade Cooling
Author: Chaitanya D Ghodke
Publisher: SAE International
ISBN: 0768095026
Category : Technology & Engineering
Languages : en
Pages : 238
Book Description
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.
Publisher: SAE International
ISBN: 0768095026
Category : Technology & Engineering
Languages : en
Pages : 238
Book Description
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.
NASA Technical Note
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 412
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 412
Book Description
ICCM/2
Author: Bryan R. Noton
Publisher:
ISBN:
Category : Composite materials
Languages : en
Pages : 874
Book Description
Publisher:
ISBN:
Category : Composite materials
Languages : en
Pages : 874
Book Description
Government Reports Announcements & Index
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1096
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1096
Book Description
Bibliography of Scientific and Industrial Reports
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1006
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1006
Book Description