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Overall Cooling Effectiveness on a Flat Plate With Both Film Cooling and Impingement Cooling in Hot Gas Condition

Volume 5A: Heat Transfer, 2016
This paper presents experimental results of temperature distribution on a flat plate with both film cooling and impingement cooling configurations. The film plate consists of 4 rows of round holes injected at an angle of 30°. The impingement plate has a 6×6 jet array.
Bo Shi   +4 more
openaire   +2 more sources

Overall cooling effectiveness of effusion cooled annular combustor liner at reacting flow conditions

Applied Thermal Engineering, 2018
Abstract A three-sector annular combustor test rig is built to carry out experimental investigation on the liner effusion cooling performance using steady state infrared radiation thermography method at reacting flow conditions. 7 rows of effusion holes in a staggered layout are distributed on both inner and outer liner bended testing plates, where ...
Yongbin Ji   +3 more
openaire   +2 more sources

Experimental Study on the Overall Cooling Effectiveness of Effusion-Cooling Ceramic Matrix Composite Platform

Journal of Thermal Science, 2023
Kun Du   +4 more
openaire   +2 more sources

Theoretical and experimental analysis of overall cooling effectiveness for afterburner double-wall heat shield

International Journal of Heat and Mass Transfer, 2021
Jiajia Niu   +4 more
exaly   +2 more sources

Effect of different internal impingement structures and cratered film cooling holes on overall cooling effectiveness

Journal of the Brazilian Society of Mechanical Sciences and Engineering
Yuhui Shen   +3 more
openaire   +2 more sources

The Effects of Channel Supplies on Overall Film-Cooling Effectiveness

Volume 7A: Heat Transfer — Combustors; Film Cooling, 2023
Abstract Cooling components in the hot section of a gas turbine is essential to component durability. Common methods of cooling include rib turbulators in internal passages and film cooling on external surfaces. The holes that produce the film cooling are fed from the internal channels often containing ribs.
Emma M. Veley   +2 more
openaire   +1 more source

Overall Cooling Effectiveness With Internal Serpentine Channels and Optimized Film Cooling Holes

Journal of Turbomachinery, 2023
Abstract The overall cooling effectiveness for gas turbine airfoils is a function of the combined cooling due to internal cooling configurations and film cooling configurations. Typically, film cooling configurations are evaluated independent of the cooling effects of the internal feed channels, generally based on adiabatic effectiveness
Christopher Yoon   +3 more
openaire   +1 more source

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