Author:
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 216
Book Description
NACA Conference on Turbine Materials and Cooling
Author:
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 216
Book Description
Publisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 216
Book Description
NACA Conference on Turbine Cooling
NACA Conference on Turbines
NACA Research Memorandum
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48
Book Description
NASA Reference Publication
Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 984
Book Description
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 984
Book Description
Fabrication and Endurance of Air-cooled Strut-supported Turbine Blades with Struts Cast of X-40 Alloy
Author: Eugene F. Schum
Publisher:
ISBN:
Category : Air-cooled engines
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Air-cooled engines
Languages : en
Pages : 48
Book Description
Survey of Advantages and Problems Associated with Transpiration Cooling and Film Cooling of Gas-turbine Blades
Author: Ernst Rudolf Georg Eckert
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
Summary: Transpiration and film cooling promise to be effective methods of cooling gas-turbine blades; consequently, analytical and experimental investigations are being conducted to obtain a better understanding of these processes. This report serves as an introduction to these cooling methods, explains the physical processes, and surveys the information available for predicting blade temperatures and heat-transfer rates. In addition, the difficulties encountered in obtaining a uniform blade temperature are discussed, and the possibilities of correcting these difficulties are indicated. Air is the only coolant considered in the application of these cooling methods.
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
Summary: Transpiration and film cooling promise to be effective methods of cooling gas-turbine blades; consequently, analytical and experimental investigations are being conducted to obtain a better understanding of these processes. This report serves as an introduction to these cooling methods, explains the physical processes, and surveys the information available for predicting blade temperatures and heat-transfer rates. In addition, the difficulties encountered in obtaining a uniform blade temperature are discussed, and the possibilities of correcting these difficulties are indicated. Air is the only coolant considered in the application of these cooling methods.
Evaluation of a Compressor Bleed System for Rim Cooling the Turbine Wheel of a Turbojet Engine
Author: C. R. Morse
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 26
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 26
Book Description
Advances in Turbine Materials, Design and Manufacturing
Author: Andrew Strang
Publisher: CRC Press
ISBN:
Category : Science
Languages : en
Pages : 814
Book Description
Proceedings of the Fourth International Charles Parsons Turbine Conference, with focus on Advances in Turbine Materials, Design and Manufacturing held on the 4-6 November 1997, at the Civic Centre, Newcastle-upon-Tyne, UK
Publisher: CRC Press
ISBN:
Category : Science
Languages : en
Pages : 814
Book Description
Proceedings of the Fourth International Charles Parsons Turbine Conference, with focus on Advances in Turbine Materials, Design and Manufacturing held on the 4-6 November 1997, at the Civic Centre, Newcastle-upon-Tyne, UK
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1440
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1440
Book Description