Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine
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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
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Author :
language : en
Publisher:
Release Date : 1981
Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine 1 Volute Manifold And Stator Performance written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1981 with categories.
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
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Author : Richard J. Roelke
language : en
Publisher:
Release Date : 1982
Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine written by Richard J. Roelke and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with categories.
Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine 3 Performance Of Redesigned Turbine
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Author :
language : en
Publisher:
Release Date : 1984
Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine 3 Performance Of Redesigned Turbine written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1984 with categories.
Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine
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Author : Richard J. Roelke
language : en
Publisher:
Release Date : 1981
Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine written by Richard J. Roelke and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1981 with Automotive gas turbines categories.
Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine 2
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-20
Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine 2 written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-20 with categories.
The aerodynamic performance of the compressor-drive turbine of the DOE upgraded gas turbine engine was determined in low temperature air. The as-received cast rotor blading had a significantly thicker profile than design and a fairly rough surface finish. Because of these blading imperfections a series of stage tests with modified rotors were made. These included the as-cast rotor, a reduced-roughness rotor, and a rotor with blades thinned to near design. Significant performance changes were measured. Tests were also made to determine the effect of Reynolds number on the turbine performance. Comparisons are made between this turbine and the compressor-drive turbine of the DOE baseline gas turbine engine. Roelke, R. J. and Haas, J. E. Glenn Research Center NASA-TM-82818, DOE/NASA/1011-36, NAS 1.15:82818, AVRADCOM-TR-82-C-1 EC-77-A-31-1011
Cold Air Performance Of The Compressor Drive Turbine Of The Department Of Energy Baseline Automobile Gas Turbine Engine
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Author : Richard J. Roelke
language : en
Publisher:
Release Date : 1978
Cold Air Performance Of The Compressor Drive Turbine Of The Department Of Energy Baseline Automobile Gas Turbine Engine written by Richard J. Roelke and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1978 with Gas-turbines categories.
Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine 1
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Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-07-20
Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine 1 written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-07-20 with categories.
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
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Author :
language : en
Publisher:
Release Date : 1984
Energy Research Abstracts written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1984 with Power resources categories.
Semiannual, with semiannual and annual indexes. References to all scientific and technical literature coming from DOE, its laboratories, energy centers, and contractors. Includes all works deriving from DOE, other related government-sponsored information, and foreign nonnuclear information. Arranged under 39 categories, e.g., Biomedical sciences, basic studies; Biomedical sciences, applied studies; Health and safety; and Fusion energy. Entry gives bibliographical information and abstract. Corporate, author, subject, report number indexes.
Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine Ii Stage Performance
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Author :
language : en
Publisher:
Release Date : 1982
Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine Ii Stage Performance written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with categories.
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).
Nasa Technical Memorandum
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Author :
language : en
Publisher:
Release Date : 1982
Nasa Technical Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with Aeronautics categories.