Results 321 to 330 of about 167,722 (364)
Some of the next articles are maybe not open access.

Improvement in Film Cooling Effectiveness Using Single and Double Rows of Holes With Adverse Compound Angle Orientations

Journal of Thermal Science and Engineering Apllications, 2018
Three-dimensional Reynolds-averaged Navier–Stokes equations with shear stress transport turbulence model are used to analyze the film cooling effectiveness on a flat plate having single row of film hole involving cylindrical hole (CH) and laidback hole
E. Kannan   +4 more
semanticscholar   +1 more source

DNS study of pulsed film cooling for enhanced cooling effectiveness

International Journal of Heat and Mass Transfer, 2009
zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Muldoon, Frank, Acharya, Sumanta
openaire   +2 more sources

Enhancement of Full Coverage Film Cooling Effectiveness with Mixed Injection Holes

International journal of turbo & jet-engines, 2018
In the present work numerical study of full coverage film cooling on an adiabatic flat plate is carried out. Cooling performance of three configurations of cylindrical holes is studied with downstream injection, upstream injection and mixed injection. In
Mukesh Prakash Mishra   +3 more
semanticscholar   +1 more source

Surface roughness effects on film-cooling effectiveness in a fan-shaped cooling hole

Aerospace Science and Technology, 2021
A. Zamiri, S. You, J. Chung
semanticscholar   +1 more source

Two-dimensional film-cooling effectiveness prediction based on deconvolution neural network

International Communications in Heat and Mass Transfer, 2021
Yaning Wang   +5 more
semanticscholar   +1 more source

Effects of Jet Geometries on Film-cooling Effectiveness

2007
Numerical simulations based on control volume method and RNG k-e turbulence model were performed to investigate the flow and heat transfer characteristics of the flat plate film cooling, squirting out from a cone-shaped jet orifice with a diffuser angle of γ to be 300 and a round-shaped jet orifice respectively.
Ling Zhang   +3 more
openaire   +1 more source

ENHANCED FILM COOLING EFFECTIVENESS USING TURBULENCE PROMOTER IN COOLING HOLE

Journal of Enhanced Heat Transfer
The film cooling is investigated experimentally and numerically for gas turbine blade cooling. Film cooling performance is vital for safe operation of the blades. By calculating the film cooling effectiveness, the effect of wall roughness through a turbulence promoter inside the cooling hole is evaluated.
E. U. Martínez-Sandoval   +3 more
openaire   +1 more source

Experimental and numerical investigations of overall cooling effectiveness on a vane endwall with jet impingement and film cooling

Applied Thermal Engineering, 2019
Xing Yang   +7 more
semanticscholar   +1 more source

Experimental investigation of film cooling effectiveness on a gas turbine blade pressure surface with diffusion slot holes

Applied Thermal Engineering, 2020
Zhiqiang Yu   +4 more
semanticscholar   +1 more source

Home - About - Disclaimer - Privacy