Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine Ii Stage Performance
DOWNLOAD
FREE 30 Days
Download Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine Ii Stage Performance PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine Ii Stage Performance book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page
Cold Air Performance Of Compressor Drive Turbine Of Department Of Energy Upgraded Automobile Gas Turbine Engine
DOWNLOAD
FREE 30 Days
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
DOWNLOAD
FREE 30 Days
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 1 Volute Manifold And Stator Performance
DOWNLOAD
FREE 30 Days
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 2
DOWNLOAD
FREE 30 Days
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
DOWNLOAD
FREE 30 Days
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
DOWNLOAD
FREE 30 Days
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 Ii Stage Performance
DOWNLOAD
FREE 30 Days
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
DOWNLOAD
FREE 30 Days
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.
Energy Research Abstracts
DOWNLOAD
FREE 30 Days
Author :
language : en
Publisher:
Release Date : 1991
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 1991 with Power resources categories.
Scientific And Technical Aerospace Reports
DOWNLOAD
FREE 30 Days
Author :
language : en
Publisher:
Release Date : 1991
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1991 with Aeronautics categories.
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.