UNCERTAINTY QUANTIFICATION ANALYSIS OF BACK FACING STEPS FILM COOLING CONFIGURATIONS

被引:0
作者
Sakai, Eiji [1 ]
Bai, Meng [2 ]
Ahlfeld, Richard [2 ]
Montomoli, Francesco [2 ]
机构
[1] Cent Res Inst Elect Power Ind, Tokyo, Kanagawa, Japan
[2] Imperial Coll London, Uncertainty Quantificat Lab, London, England
来源
PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 5A | 2018年
关键词
HOLES; GEOMETRY; DENSITY; ROW;
D O I
暂无
中图分类号
O414.1 [热力学];
学科分类号
摘要
This paper compares two back step film-cooling configurations under an uncertainty quantification framework. An important limit of such configurations is their reliability under geometrical variations, which is taken into account in this study. For the back step configurations, a straight and a curved step is used. Detached eddy simulations with k-co turbulence model are performed using OpenFOAM ver. 4.0. The Reynolds number is based on the main stream velocity and film cooling hole diameter, d, and is Re=15,300. The investigated step heights are 0.5d and 0.75d, and the blowing ratios, BR, are 0.5 and 1.0. The straight and the curved steps are found to enhance lateral spreading of coolant flow, resulting in higher film cooling effectiveness compared to the baseline case without the step at comparatively higher BR conditions. The curved step shows better performance than the straight one in particular from BR=1.0 upwards with the step height of 0.5d. At lower BR with lower Hld, and at higher BR with higher Hld, deterministic simulations are not able to identify the best performer. However when the performance of the two configurations is evaluated considering the stochastic variation of step height and the cooling condition, the benefit of the curved step becomes clear. In particular, the curved step shows better mean performance and has a higher probability to achieve a better performance than the other one. The uncertainty in the film cooling effectiveness caused by the uncertainty of the step height and the BR is investigated using Sparse Approximation of Moment-Based Arbitrary polynomial chaos (SAMBA).
引用
收藏
页数:12
相关论文
共 14 条
[1]   SAMBA: Sparse Approximation of Moment-Based Arbitrary Polynomial Chaos [J].
Ahlfeld, R. ;
Belkouchi, B. ;
Montomoli, F. .
JOURNAL OF COMPUTATIONAL PHYSICS, 2016, 320 :1-16
[2]  
[Anonymous], 1963, Dokl. Akad. Nauk SSSR
[3]   A review of shaped hole turbine film-cooling technology [J].
Bunker, RS .
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2005, 127 (04) :441-453
[4]   THE FLOW AND FILM COOLING EFFECTIVENESS FOLLOWING INJECTION THROUGH A ROW OF HOLES [J].
FOSTER, NW ;
LAMPARD, D .
JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1980, 102 (03) :584-588
[5]   EFFECTS OF HOLE GEOMETRY AND DENSITY ON 3-DIMENSIONAL FILM COOLING [J].
GOLDSTEIN, RJ ;
ECKERT, ERG ;
BURGGRAF, F .
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1974, 17 (05) :595-607
[6]  
Kawabata H., 2015, GT201544026 ASME
[7]   Adiabatic effectiveness, thermal fields, and velocity fields for film cooling with large angle injection [J].
Kohli, A ;
Bogard, DG .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1997, 119 (02) :352-358
[8]   Effect of Trench Width and Depth on Film Cooling From Cylindrical Holes Embedded in Trenches [J].
Lu, Yiping ;
Dhungel, Alok ;
Ekkad, Srinath V. ;
Bunker, Ronald S. .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2009, 131 (01)
[9]   Numerical and experimental investigation of a new film cooling geometry with high P/D ratio [J].
Montomoli, F. ;
D'Ammaro, A. ;
Uchida, S. .
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2013, 66 :366-375
[10]   Increasing adiabatic film-cooling effectiveness by using an upstream ramp [J].
Na, Sangkwon ;
Shih, Tom I-P. .
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2007, 129 (04) :464-471