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

Download or read book 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 published by . This book was released on 1981 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).

Book Cold Air Performance of Compressor Drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine  2

Download or read book 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 published by Createspace Independent Publishing Platform. This book was released on 2018-07-20 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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

Book Cold air Performance of the Compressor drive Turbine of the Department of Energy Baseline Automobile Gas turbine Engine

Download or read book Cold air Performance of the Compressor drive Turbine of the Department of Energy Baseline Automobile Gas turbine Engine written by Richard J. Roelke and published by . This book was released on 1978 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

Download or read book Cold Air Performance of Compressor Drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine II Stage Performance written by and published by . This book was released on 1982 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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).

Book NASA Technical Memorandum

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1982 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Cold air Performance of Compressor drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine  3  Performance of Redesigned Turbine

Download or read book Cold air Performance of Compressor drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine 3 Performance of Redesigned Turbine written by and published by . This book was released on 1984 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Energy Research Abstracts

Download or read book Energy Research Abstracts written by and published by . This book was released on 1983 with total page 1228 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Cold air Performance of Compressor drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine

Download or read book Cold air Performance of Compressor drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine written by Richard J. Roelke and published by . This book was released on 1981 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1984 with total page 1278 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Energy

    Book Details:
  • Author :
  • Publisher :
  • Release : 1983
  • ISBN :
  • Pages : 322 pages

Download or read book Energy written by and published by . This book was released on 1983 with total page 322 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Energy  a Continuing Bibliography with Indexes

Download or read book Energy a Continuing Bibliography with Indexes written by and published by . This book was released on 1979 with total page 890 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Monthly Catalogue  United States Public Documents

Download or read book Monthly Catalogue United States Public Documents written by and published by . This book was released on 1985 with total page 1426 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Cold air Performance of Compressor drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine

Download or read book Cold air Performance of Compressor drive Turbine of Department of Energy Upgraded Automobile Gas Turbine Engine written by Richard J. Roelke and published by . This book was released on 1981 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Abstract Bulletin

Download or read book Technical Abstract Bulletin written by and published by . This book was released on 1981 with total page 224 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

Download or read book 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 published by Createspace Independent Publishing Platform. This book was released on 2018-07-20 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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