A transient liquid crystal technique was used to measure the local heat transfer coefficients on a target surface with array impingement hole. The effects of jet Reynolds numbers (5000
10000
15000
20000) and the ratios of the side bleeding(0
0.25
0.4
0.6
0.8
1) on the heat transfer coefficients were investigated. Results show that
the heat transfer coefficients on the target surface rise with the increase of jet Reynolds number; the heat transfer coefficients on the impingement stagnation regions are the highest
and the heat transfer coefficients on the film holes regions are also relatively high. The average heat transfer coefficients on the target surface decrease with the increase of the ratio of the side bleeding
and are not strongly influenced with the low ratio of side bleeding
but significantly affected with the high ratio of side bleeding.
Heat transfer measurements of turn-over channel in turbine blade
Influence of exit flow type on heat transfer of array impingement
Experiment of the effects of geometrical parameters on internalheat transfer in an impinging contraction channel with liquid crystal transient technique
Numerical simulation of spoiler ring’s effect on combustion and flow of powdered rocket motor
Pressure loss and heat transfer characteristics experiment of swirling impinging jet with different shape nozzles
Related Author
WANG Xiao-zeng
ZHANG Li
ZHU Hui-ren
LIANG Wei-ying
LI Zhong-zhou
ZHOU Lei-sheng
ZHANG Xia
LI Chun-lin
Related Institution
School of Power and Energy, Northwestern Polytechnical University