Results 11 to 20 of about 328,216 (310)

Effect of main stream turbulence on the film cooling effectiveness of a circular and a fan-shaped film cooling hole

open access: yesMechanical 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

Experimental study on heat transfer and throughflow losses characteristics of single/triple-row holes with an engine-representative density ratio

open access: yesCase Studies in Thermal Engineering, 2021
In present study, the heat transfer and the throughflow losses characteristics of single/triple-row of fan-shaped and cylindrical film cooling holes with a fixed outlet width are studied experimentally with an engine-representative density ratio.
H. Wei, Y.Q. Zu
doaj   +1 more source

The Combined Influences of Film Cooling and Thermal Barrier Coatings on the Cooling Performances of a Film and Internal Cooled Vane [PDF]

open access: yesCoatings, 2020
This paper presents a numerical investigation on the combined influences of film cooling and thermal barrier coatings (TBCs) on the cooling performances of a NASA C3X guide vane. The results show that: (1) film cooling on the pressure side is more effective than suction side, especially on the trailing edge where multiple cooling and thermal protection
Li Shi, Zhiying Sun, Yuanfeng Lu
openaire   +1 more source

Experimental investigation of the film cooling performance by triangular-shaped thin plates on inclined cylindrical holes

open access: yesFrontiers in Energy Research, 2022
Experimental investigations have been conducted to improve the cooling effectiveness of film-cooling technology. A multiple row of cylindrical holes at the flat surface was considered by inclining the holes at 35° along the streamwise direction.
Jaemun Choi   +5 more
doaj   +1 more source

Film-cooling hole optimization and experimental validation considering the lateral pressure gradient

open access: yesFrontiers in Mechanical Engineering, 2023
The flow in the turbine endwall region consists of the complicated secondary flow structures driven by the lateral pressure gradient, which heavily affects the performance of film cooling.
Hao Zhang   +4 more
doaj   +1 more source

Uncertainty quantification and film cooling

open access: yesComputers & Fluids, 2013
zbMATH Open Web Interface contents unavailable due to conflicting licenses.
D'Ammaro, A, Montomoli, F
openaire   +5 more sources

Study on the effect of waveform film holes on film cooling efficiency

open access: yesFrontiers in Energy Research, 2023
In order to improve the film cooling efficiency of the cooling gas on the hot side wall of the plate, the flow field, temperature field and the average film cooling efficiency of the cylindrical hole, rectangular hole and waveform hole near the wall were
Cheng Qian   +4 more
doaj   +1 more source

Effects of Turbulence Promoters of Gas Turbine Blades on Film Cooling Performance

open access: yesJournal 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

Numerical study on the cooling characteristics of cat-ear-shaped film-cooling holes on turbine blades

open access: yesCase Studies in Thermal Engineering, 2022
The turbine blade cooling technology is developing rapidly, with film cooling being the focus of research. To address the problems of poor cooling performance and low cooling efficiency of existing film holes, this paper proposes a hole structure of cat ...
Lihao Zhang   +4 more
doaj   +1 more source

Experimental Study on the Improvement of the Film Cooling Effectiveness of Various Modified Configurations Based on a Fan-Shaped Film Cooling Hole on a Flat Plate

open access: yesEnergies, 2023
Modern gas turbines have evolved by increasing the turbine inlet temperature (TIT) to improve performance. This development has led to a demand for cooling techniques.
Seokmin Kim   +3 more
doaj   +1 more source

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