Steam Turbine and Gas Turbine
ZHANG Ling, GUO Ruihong, LI Hao, GUO Dafei
2015, 35(4): 280-286.
By steady state calculation using Fluent segregated implicit solver, and in combination with Realizable k-ε turbulence model, numerical simulations were conducted to the film cooling effectiveness on a flat plate respectively with cylindrical, single-inlet double-outlet and sister holes at blowing ratios of 0.5, 1.0, 1.5 and 2.0, so as to study the film cooling effectiveness in main stream and lateral direction as well as to study the flow field. Results show that along the main stream direction, the cooling efficiency of sister holes is higher than that of single-inlet double-outlet hole in the near region of hole, and their difference increases with the rise of blowing ratio; but in the far region of hole, the cooling efficiency of sister holes drops a little and becomes lower than the single-inlet double-outlet hole, due to the earlier wall attachment of jet and the momentum loss caused by the mix of jet with main stream. Whereas along the lateral direction, the cooling film of sister holes is relatively uniform in the near region of hole, and the cooling effectiveness of single-inlet double-outlet hole is good at one side and poor at the other side in the far region of hole, due to the film displacement caused by jet velocity difference of the primary and secondary hole. It is concluded that the cooling effectiveness of single-inlet double-outlet hole is better in the case of lower blowing ratios, while the cooling effectiveness of sister holes becomes better in the case of higher blowing ratios.