ZHANG Wei, LI Guang-chao, PENG Da-wei, et al. Influence of rotation on discharge coefficients of two rows of film holes in channel with rib turbulators[J]. 2010, 25(6).
DOI:
ZHANG Wei, LI Guang-chao, PENG Da-wei, et al. Influence of rotation on discharge coefficients of two rows of film holes in channel with rib turbulators[J]. 2010, 25(6).DOI:
Influence of rotation on discharge coefficients of two rows of film holes in channel with rib turbulators
In order to understand the bleed performance of the film hole on the internal tunnel within the blade
the influence of the rotation on the discharge coefficients of film holes in rectangular channel with both rib-roughened wall and two rows of film hole suctions was studied by numerical simulation at Reynolds number 60000
rotation number 0
0.11 and 0.22
and suction ratio of 0.22.The numerical results agreed well with the experimental data in the stationary passages.The averaged discharge coefficients of the two holes increase by 90% in the clockwise rotating channel and decrease by 10% in the counter-clockwise channel.The discharge coefficients of the left holes are 4~5 times the right holes in the event of clockwise rotation.The discharge coefficients of the left holes and the right holes differ little in the event of counter-clockwise rotation.
Numerical Investigation of Influence of Rib Orientation on Discharge Coefficients
Influence physics of mainstream pressure gradient on film hole discharge coefficient
PIV measurement of flow field for tip clearance flow in turbine shroud
Effect of the shape of divider wall on heat transfer and flow resistance characteristic of passage
Influence of orientation angles of branch hole on film cooling effectiveness with one inlet and double outlet hole injection
Related Author
NI Meng
ZHU Hui-ren
QIU Yun Ding
LIU Song-ling
ZHU Hui-ren
LUO Jian-xia
HUANG Xiao-yang
LIU Zhi-gang
Related Institution
University of Hong Kong,Hong KongChina
Northwestern Polytechnical University
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
School of Energy and Mechanical Engineering, North China Electric Power University