Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine 1 Volute Manifold And Stator Performance

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Cold-air Performance of Compressor-drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine. 1: Volute-manifold and Stator Performance

Anonim
Cold air Performance of Compressor drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine 1 Volute manifold and Stator Performance Book PDF

Author : Anonim
Publisher : Unknown
Page : 24 pages
File Size : 50,8 Mb
Release : 1981
Category : Electronic
ISBN : NASA:31769000551823

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Cold-air Performance of Compressor-drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine. 1: Volute-manifold and Stator Performance by Anonim Pdf

The aerodynamic performance of the inlet manifold and stator assembly of the compressor-drive turbine was experimentally determined with cold air as the working fluid. The investigation included measurements of mass flow and stator-exit fluid torque as well as radial surveys of total pressure and flow angle at the stator inlet and annulus surveys of total pressure and flow angle at the stator exit. The stator-exit aftermixed flow conditions and overall stator efficiency were obtained and compared with their design values and the experimental results from three other stators. In addition, an analysis was made to determine the constituent aerodynamic losses that made up the stator kinetic energy loss. (Author).

Cold-Air Performance of Compressor-Drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine. 1

National Aeronautics and Space Administration (NASA)
Cold Air Performance of Compressor Drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine 1 Book PDF

Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 24 pages
File Size : 48,6 Mb
Release : 2018-07-20
Category : Electronic
ISBN : 1723398764

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Cold-Air Performance of Compressor-Drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine. 1 by National Aeronautics and Space Administration (NASA) Pdf

The aerodynamic performance of the inlet manifold and stator assembly of the compressor drive turbine was experimentally determined with cold air as the working fluid. The investigation included measurements of mass flow and stator-exit fluid torque as well as radial surveys of total pressure and flow angle at the stator inlet and annulus surveys of total pressure and flow angle at the stator exit. The stator-exit aftermixed flow conditions and overall stator efficiency were obtained and compared with their design values and the experimental results from three other stators. In addition, an analysis was made to determine the constituent aerodynamic losses that made up the stator kinetic energy loss. Roelke, R. J. and Haas, J. E. Glenn Research Center NASA-TM-82682, DOE/NASA/1011-34, E-572, AVRADCOM-TR-80-C-20 EC-77-A-31-1011; RTOP 505-32-2B

Energy Research Abstracts

Anonim
Energy Research Abstracts Book PDF

Author : Anonim
Publisher : Unknown
Page : 402 pages
File Size : 55,5 Mb
Release : 1981
Category : Power resources
ISBN : MINN:30000010513939

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Energy Research Abstracts by Anonim Pdf

NASA Technical Memorandum

Anonim
NASA Technical Memorandum Book PDF

Author : Anonim
Publisher : Unknown
Page : 28 pages
File Size : 52,5 Mb
Release : 1982
Category : Aeronautics
ISBN : MINN:319510008452917

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NASA Technical Memorandum by Anonim Pdf

Technical Abstract Bulletin

Anonim
Technical Abstract Bulletin Book PDF

Author : Anonim
Publisher : Unknown
Page : 224 pages
File Size : 55,5 Mb
Release : 1981
Category : Science
ISBN : CORNELL:31924057177549

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Technical Abstract Bulletin by Anonim Pdf

Cold-Air Performance of Compressor-Drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine. II. Stage Performance

Anonim
Cold Air Performance of Compressor Drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine II Stage Performance Book PDF

Author : Anonim
Publisher : Unknown
Page : 28 pages
File Size : 48,6 Mb
Release : 1982
Category : Electronic
ISBN : UIUC:30112008540574

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Cold-Air Performance of Compressor-Drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine. II. Stage Performance by Anonim Pdf

The aerodynamic performance of the compressor-drive turbine of the DOE Upgraded Gas Turbine (UGT) engine was determined in low-temperature air. The nominal turbine-inlet temperature was 320 K. Inlet pressures were varied between 0.4 and 2.4 bars absolute. The turbine blading used in these tests consisted of duplicates of the stator and rotor castings used in development engine tests. The as-received cast rotor blades had a significantly thicker profile than design and a fairly rough surface finish. Because of these blade profile imperfections three turbine rotor configurations were evaluated. These were the as-cast rotor, a reduced-roughness rotor, and a rotor with the blade profiles thinned to near the design profile. Tests to determine the effect of Reynolds number on the turbine performance were also made. (Author).

Government reports annual index

Anonim
Government reports annual index Book PDF

Author : Anonim
Publisher : Unknown
Page : 940 pages
File Size : 47,5 Mb
Release : 199?
Category : Electronic
ISBN : MSU:31293017237904

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Government reports annual index by Anonim Pdf

SRIM Index

Anonim
SRIM Index Book PDF

Author : Anonim
Publisher : Unknown
Page : 502 pages
File Size : 42,6 Mb
Release : 1982
Category : Computer programming
ISBN : UCAL:$C53954

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SRIM Index by Anonim Pdf