Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
Effect of Coolant Flow Ejection on Aerodynamic Performance of Low-aspect-ratio Vanes. 2: Performance with Coolant Flow Ejection at Temperature Ratios Up to 2
Effect of Coolant Flow Ejection on Aerodynamic Performance of Low-aspect-ratio Vanes
Author: Jeffrey E. Haas
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38
Book Description
Effect of Coolant Flow Ejection on Aerodynamic Performance of Low-Aspect-Ratio Vanes. 2
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725671096
Category :
Languages : en
Pages : 36
Book Description
The aerodynamic performance of a 0.5 aspect ratio turbine vane configuration with coolant flow ejection was experimentally determined in a full annular cascade. The vanes were tested at a nominal mean section ideal critical velocity ratio of 0.890 over a range of primary to coolant total temperature ratio from 1.0 to 2.08 and a range of coolant to primary total pressure ratio from 1.0 to 1.4 which corresponded to coolant flows from 3.0 to 10.7 percent of the primary flow. The variations in primary and thermodynamic efficiency and exit flow conditions with circumferential and radial position were obtained. Hass, J. E. and Kofskey, M. G. Glenn Research Center NASA-TP-1057, E-9213 RTOP 505-04...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725671096
Category :
Languages : en
Pages : 36
Book Description
The aerodynamic performance of a 0.5 aspect ratio turbine vane configuration with coolant flow ejection was experimentally determined in a full annular cascade. The vanes were tested at a nominal mean section ideal critical velocity ratio of 0.890 over a range of primary to coolant total temperature ratio from 1.0 to 2.08 and a range of coolant to primary total pressure ratio from 1.0 to 1.4 which corresponded to coolant flows from 3.0 to 10.7 percent of the primary flow. The variations in primary and thermodynamic efficiency and exit flow conditions with circumferential and radial position were obtained. Hass, J. E. and Kofskey, M. G. Glenn Research Center NASA-TP-1057, E-9213 RTOP 505-04...
NASA Technical Paper
NASA Technical Paper
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 578
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 578
Book Description
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 832
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 832
Book Description
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1228
Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1228
Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index