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 PDF Download

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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. 2: Performance with Coolant Flow Ejection at Temperature Ratios Up to 2 PDF 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. 2: Performance with Coolant Flow Ejection at Temperature Ratios Up to 2 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 40

Book Description


Effect of Coolant Flow Ejection on Aerodynamic Performance of Low-aspect-ratio Vanes

Effect of Coolant Flow Ejection on Aerodynamic Performance of Low-aspect-ratio Vanes PDF Author: Jeffrey E. Haas
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 38

Book Description


Effect of Coolant Flow Ejection on Aerodynamic Performance of Low-Aspect-Ratio Vanes. 2

Effect of Coolant Flow Ejection on Aerodynamic Performance of Low-Aspect-Ratio Vanes. 2 PDF 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...

NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 40

Book Description


NASA Technical Paper

NASA Technical Paper PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 578

Book Description


Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 832

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF 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

NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 384

Book Description


NASA Scientific and Technical Publications

NASA Scientific and Technical Publications PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 410

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1018

Book Description