Large Eddy Simulations for Film Cooling Assessment of Cylindrical and Laidback Fan-Shaped Holes With Reverse Injection

被引:12
|
作者
Singh, Ashutosh Kumar [1 ]
Singh, Kuldeep [2 ]
Singh, Dushyant [1 ]
Sahoo, Niranjan [3 ]
机构
[1] Natl Inst Technol Manipur, Dept Mech Engn, Imphal 795004, Manipur, India
[2] Univ Nottingham, Gas Turbine & Transmiss Res Ctr, Nottingham NG7 2TU, England
[3] Indian Inst Technol, Dept Mech Engn, Gauhati 781039, Assam, India
关键词
film cooling; large eddy simulations; cylindrical hole; shaped hole; TURBULENT FLOWS; BLOWING RATIO; DENSITY; JET;
D O I
10.1115/1.4048679
中图分类号
O414.1 [热力学];
学科分类号
摘要
The large eddy simulations (LES) are performed to access the film cooling performance of cylindrical and reverse shaped hole for forward and reverse injection configurations. In the case of reverse/backward injection, the secondary flow is injected in such a way that its axial velocity component is in the direction opposite to mainstream flow. The study is carried out for a blowing ratio (M = 1), density ratio (DR = 2.42), and injection angle (alpha = 35 deg). Formation of counter-rotating vortex pair (CRVP) is one of the major issues in the film cooling. This study revealed that the CRVP found in the case of forward cylindrical hole which promotes coolant jet "liftoff" is completely mitigated in the case of the reverse shaped hole. The coolant coverage for reverse cylindrical and reverse shaped holes is uniform and higher. The reverse shaped hole shows promising results among investigated configurations. The lateral averaged film cooling effectiveness of reverse shaped hole is 1.16-1.42 times higher as compared to the forward shaped holes. The improvement in the lateral averaged film cooling effectiveness of reverse cylindrical hole (RCH) injection over forward cylindrical hole (FCH) injection is 1.33-2 times.
引用
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页数:16
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