Results 11 to 20 of about 4,477,602 (248)
Turbine cooling and heat transfer modelling for gas turbine performance simulation [PDF]
, 2015 The successful design of cooling systems for gas turbine engines is a key factor to feasibility of new projects, as the trend for increasing turbine entry temperatures implies requirements for more sophisticated cooling methods.
Apostolidis, Asteris
core +7 more sources
Enhancement of Film Cooling Effectiveness in a Supersonic Nozzle. [PDF]
Entropy (Basel), 2023 Film cooling as applied to rocket nozzles is analyzed numerically with emphasis on the assessment of the effect of the mixing of coolant with the hot stream.
Somasekharan N +5 more
europepmc +2 more sources
Local Heat Transfer Measurements on a Rotating Flat Blade Model with a Single Film Hole [PDF]
, 2009 An experimental study was performed to measure the heat transfer coefficient distributions on a flat blade model under rotating operating conditions. A steady-state thermochromic liquid crystal technique was employed to measure the surface temperature ...
Tao, Zhi +8 more
core +1 more source
Energies, 2022 In this paper, flat plate film cooling with two rows of compound angle cylindrical film cooling holes was investigated. A data processing method was evaluated which could determine the film cooling effectiveness and heat transfer coefficient ...
Mingjie Zhang
doaj +1 more source
, 2022 In this paper, the effects of internal coolant crossflow on double-jet holes were simulated and compared with two rows of cylindrical holes under three blowing ratios (M = 0.5, 1.0, and 1.5), with an established and validated turbulence model.
Xie, Gongnan, +4 more
core +1 more source
Mechanical Engineering Journal, 2020 The reliability of turbine blades and vanes of modern high temperature gas turbines is assured by turbine blade cooling technologies. Among the various cooling methods, film cooling has been a key technology to ensure the long-term operation of turbine ...
Kenichiro TAKEISHI +3 more
doaj +1 more source
Convective and Film Cooled Nozzle Extension for a High Pressure Rocket Subscale Combustion Chamber [PDF]
, 2010 Experimental investigations have been carried out to study heat transfer, flow separation, and side loads in a subscale nozzle extension. A Vulcain 2-like nozzle geometry has been tested with combustion chamber pressures up to 13 MPa. A new manufacturing
Richard Arnold +5 more
core +1 more source
Effects of Turbulence Promoters of Gas Turbine Blades on Film Cooling Performance
Journal of Thermal Science and Technology, 2012 The effects of orientation of turbulence promoting ribs in the internal cooling air passage on the film cooling performance of outer surface of gas turbine blades have been studied experimentally.
Yukiko AGATA +3 more
doaj +1 more source
Experimental investigation of film cooling effectiveness on gas turbine blades [PDF]
, 2009 The hot gas temperature in gas turbine engines is far above the permissible metal temperatures. Advanced cooling technologies must be applied to cool the blades, so they can withstand the extreme conditions.
Gao, Zhihong
core +3 more sources
Applied Sciences, 2017 The effects of dielectric barrier discharge (DBD) plasma on the film cooling effectiveness of a 30-degree slot was experimentally investigated in a low-speed wind tunnel.
Ye Jee Kim +3 more
doaj +1 more source