Film-cooling effectiveness of rectangular diffusion holes under an inclination angle α = 45 deg, an orientation angle β = 45 deg, and a length-to-diameter ratio of L/D = 8.5 were, respectively, examined in a flat-plate experimental facility using the pressure sensitive paint (PSP) technique. Experiments were performed at a density ratio of DR = 1.38 and a mainstream turbulence intensity of Tu = 3.5%. The semicircle sidewall rectangular diffusion hole varied at three cross-sectional aspect ratios, i.e., AS = 3.4, 4.9, and 6.6. The tested results were compared with the baseline design with an inclination angle α = 30 deg, an orientation angle β = 0 deg, and a length-to-diameter ratio L/D = 6. A three-dimensional (3D) numerical simulation method was employed to analyze the flow field. The experimental results showed that the increased inclination angle converted the bi- or tri-peak effectiveness pattern of the baseline design to a single-peak pattern, weakened the lateral diffusion of coolant, and consequently decreased cooling effectiveness obviously. The decreased magnitude amplified with the increase of cross-sectional aspect ratio and blowing ratio. The adding of orientation angle seriously weakened the cooling effectiveness of the baseline design, and the blowing ratio and cross-sectional aspect ratio had almost no effect on overall cooling effectiveness. The elongated hole length provided a uniform distribution of lateral cooling effectiveness, which produced differential effects on the bi- or tri-peak pattern. The elongated hole length decreased the cooling effectiveness on the near hole region, but had less effects on overall cooling effectiveness, except the high blowing ratio.
Skip Nav Destination
Article navigation
July 2018
Research-Article
Effects of Inclination Angle, Orientation Angle, and Hole Length on Film Cooling Effectiveness of Rectangular Diffusion Holes
Bai-Tao An,
Bai-Tao An
Institute of Engineering Thermophysics,
Chinese Academy of Sciences,
Beijing 100190, China
e-mail: anbt@mail.etp.ac.cn
Chinese Academy of Sciences,
Beijing 100190, China
e-mail: anbt@mail.etp.ac.cn
Search for other works by this author on:
Jian-Jun Liu,
Jian-Jun Liu
Institute of Engineering Thermophysics,
Chinese Academy of Sciences,
Beijing 100190, China
Chinese Academy of Sciences,
Beijing 100190, China
Search for other works by this author on:
Si-Jing Zhou
Si-Jing Zhou
Institute of Engineering Thermophysics,
Chinese Academy of Sciences,
Beijing 100190, China
Chinese Academy of Sciences,
Beijing 100190, China
Search for other works by this author on:
Bai-Tao An
Institute of Engineering Thermophysics,
Chinese Academy of Sciences,
Beijing 100190, China
e-mail: anbt@mail.etp.ac.cn
Chinese Academy of Sciences,
Beijing 100190, China
e-mail: anbt@mail.etp.ac.cn
Jian-Jun Liu
Institute of Engineering Thermophysics,
Chinese Academy of Sciences,
Beijing 100190, China
Chinese Academy of Sciences,
Beijing 100190, China
Si-Jing Zhou
Institute of Engineering Thermophysics,
Chinese Academy of Sciences,
Beijing 100190, China
Chinese Academy of Sciences,
Beijing 100190, China
1Corresponding author.
Contributed by the International Gas Turbine Institute (IGTI) of ASME for publication in the JOURNAL OF TURBOMACHINERY. Manuscript received August 1, 2017; final manuscript received April 27, 2018; published online June 14, 2018. Assoc. Editor: Kenichiro Takeishi.
J. Turbomach. Jul 2018, 140(7): 071003 (13 pages)
Published Online: June 14, 2018
Article history
Received:
August 1, 2017
Revised:
April 27, 2018
Citation
An, B., Liu, J., and Zhou, S. (June 14, 2018). "Effects of Inclination Angle, Orientation Angle, and Hole Length on Film Cooling Effectiveness of Rectangular Diffusion Holes." ASME. J. Turbomach. July 2018; 140(7): 071003. https://doi.org/10.1115/1.4040101
Download citation file:
Get Email Alerts
Cited By
Characteristics of Deterministic and Stochastic Unsteadiness of Trailing Edge Cutback Film Cooling Flows
J. Turbomach (January 2025)
Related Articles
Film Cooling Effectiveness and Heat Transfer Coefficient Distributions Around Diffusion Shaped Holes
J. Heat Transfer (October,2002)
Film Cooling Effectiveness and Heat Transfer on the Trailing Edge Cutback of Gas Turbine Airfoils With Various Internal Cooling Designs
J. Turbomach (January,2006)
Comparison of Film Effectiveness and Cooling Uniformity of Conical and Cylindrical-Shaped Film Hole With Coolant-Exit Temperature Correction
J. Thermal Sci. Eng. Appl (September,2011)
Film Cooling From a Row of Holes Supplemented With Antivortex Holes
J. Turbomach (April,2009)
Related Proceedings Papers
Related Chapters
Adding Surface While Minimizing Downtime
Heat Exchanger Engineering Techniques
Natural Gas Transmission
Pipeline Design & Construction: A Practical Approach, Third Edition
Aerodynamic Performance Analysis
Axial-Flow Compressors