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Keywords: turbines
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Proceedings Papers

Proc. ASME. GT2021, Volume 4: Controls, Diagnostics, and Instrumentation; Cycle Innovations; Cycle Innovations: Energy Storage; Education; Electric Power, V004T06A003, June 7–11, 2021
Paper No: GT2021-59013
... aerodynamics turbines cascades Mach number organic Rankine cycle asymptotic expansion Abstract Abstract Results are presented of a theoretical and experimental study dealing with critical and choking Mach numbers of organic vapor flows through turbine cascades. A correlation...
Proceedings Papers

Proc. ASME. GT2020, Volume 2E: Turbomachinery, V02ET39A026, September 21–25, 2020
Paper No: GT2020-16097
...PHYSICAL QUANTITY SYNERGY IN THE INTERNAL FLOW FIELD AND APPLICATION IN RADIAL-INFLOW TURBINES Ziyi Shao1,2, Xuehui Zhang1,2,3, Xing Wang1,3, Yangli Zhu1,2,3, Wen Li1,2,3, Haisheng Chen1,2,3 1 Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing, China. 2 School...
Proceedings Papers

Proc. ASME. GT2020, Volume 6: Education; Electric Power, V006T08A009, September 21–25, 2020
Paper No: GT2020-16028
...INTERACTIVE LEARNING PLATFORM FOR TURBINE DESIGN USING REDUCED ORDER METHODS Igor Oliveira1, George Patton Silva1, Daniel Tonon1, Cleverson Bringhenti1, Jesuíno Takachi Tomita1 1Aeronautics Institute of Technology, Department of Turbomachines, São José dos Campos, SP, Brazil ABSTRACT This work...
Topics: Design, Turbines
Proceedings Papers

Proc. ASME. GT2009, Volume 7: Turbomachinery, Parts A and B, 1497-1508, June 8–12, 2009
Paper No: GT2009-59055
...”, whose details are still not well defined or understood, points to a realization that a new look at some previously unrecognized findings is needed to explain problems encountered in operation of compressors and turbines. The purpose of this paper is to call attention of the turbo-machinery community...
Proceedings Papers

Proc. ASME. GT2008, Volume 4: Heat Transfer, Parts A and B, 825-835, June 9–13, 2008
Paper No: GT2008-50901
... 04 08 2009 Deposition on film-cooled turbine components was studied in an accelerated test facility. The accelerated deposition facility seeds a natural-gas burning combustor with finely-ground coal ash particulate at 1180°C and 180 m/s ( M = 0.25). Both cylindrical and shaped holes...
Proceedings Papers

Proc. ASME. GT2007, Volume 4: Turbo Expo 2007, Parts A and B, 1365-1376, May 14–17, 2007
Paper No: GT2007-27531
... 10 03 2009 Four series of tests were performed in an accelerated deposition test facility to study the independent effects of particle size, gas temperature, and metal temperature on ash deposits from two candidate power turbine synfuels. The facility matches the gas temperature...
Proceedings Papers

Proc. ASME. GT2005, Volume 1: Turbo Expo 2005, 411-419, June 6–9, 2005
Paper No: GT2005-68479
... 03 11 2008 Ash deposits from four candidate power turbine synfuels were studied in an accelerated deposition test facility. The facility matches the gas temperature and velocity of modern first stage high pressure turbine vanes. A natural-gas combustor was seeded with finely-ground...
Proceedings Papers

Proc. ASME. GT2006, Volume 3: Heat Transfer, Parts A and B, 1055-1063, May 8–11, 2006
Paper No: GT2006-91246
... 11 09 2008 Turbine blade coupons with three different surface treatments were exposed to deposition conditions in an accelerated deposition facility. The facility simulates the flow conditions at the inlet to a first stage high pressure turbine (T = 1150°C, M = 0.31). The combustor...
Proceedings Papers

Proc. ASME. GT2006, Volume 3: Heat Transfer, Parts A and B, 1075-1082, May 8–11, 2006
Paper No: GT2006-91257
... 11 09 2008 A TBC-coated turbine blade coupon was exposed to successive deposition in an accelerated deposition facility simulating flow conditions at the inlet to a first stage high pressure turbine (T = 1150°C, M = 0.31). The combustor exit flow was seeded with dust particulate...