Abstract
Unsteady flow characteristic and film cooling effect in the blade trailing edge cutback region are numerically investigated using DES (detached eddy simulation) method at three blowing ratios, four lip thickness ratios and three rib geometries. With the experimental data, reliability and accuracy of the numerical methods are validated. The results indicate that, compared with RANS (Reynolds-averaged Navier-Stokes) equations solutions, the DES method has a superior accuracy in predicting the film cooling effectiveness on trailing-edge cutback. The lip thickness has a pronounced effect on shedding vortex scale downstream the slot. As the lip thickness ratio decreases, the film cooling effect on trailing edge cutback is improved. Compared with the line ribs, the arrangement of pin fin ribs enhances the uniformity of coolant coverage on trailing edge cutback along lateral direction. However, with different types of rib, the film cooling effectiveness on the trailing edge cutback is mainly determined by the stable cooling flow structures and mixing effect between mainstream and coolant. The development of vortex system downstream the slot is significantly affected by the blowing ratio, which in turn influences the film cooling effect on trailing edge cutback.
Similar content being viewed by others
References
M. E. Taslim, S. D. Spring and B. P. Mehlmann, Experimental investigation of film cooling effectiveness for slot of various exit geometries, Journal of Thermophysics and Heat Transfer, 6 (2) (1992) 302–307.
S. D. Holloway, J. H. Leylek and F. A. Buck, Pressure-side bleed film cooling: part II -Unsteady framework for experimental and computational results, ASME Paper No. GT 2002-30472.
P. Martini and A. Shulz, Experimental and numerical investigation of trailing edge film cooling by circular coolant wall jets ejected from a slot with internal rib arrays, ASME Journal of Turbomachinery, 126 (2004) 229–236.
P. Martini, A. Schulz and H. J. Bauer, Film cooling effectiveness and heat transfer on the trailing edge cutback of gas turbine airfoils with various internal cooling designs, Journal of Turbomachinery, 128 (1) (2006) 196–205.
P. Martini, A. Schulz, H. J. Bauer and C. F. Whitney, Detached eddy simulation of film cooling performance on the trailing edge cutback of gas turbine airfoils, ASME Journal of Turbomachinery, 128 (2) (2006)292–299.
P. Martini, Filmkühlung hochbeanspruchter turbinenschaufelhinterkanten: Wärmeübergang und strömung im nahfeld praxisbezogener ausblasespalte, Logos Verlag (2008).
F. J. Cunha and M. K. Chyu, Trailing-edge cooling for gas turbines, Journal of Propulsion and Power, 22 (2) (2006) 286–300.
F. E. Ames, N. J. Fiala and J. D. Johnson, Gill slot trailing edge heat transfer: Effects of blowing rate, reynolds number, and external turbulence on heat transfer and film cooling effectiveness, ASME Paper No. GT 2007-27397.
N. J. Fiala, I. Jaswal and F. E. Ames, Letterbox trailing edge heat transfer: Effects of blowing rate, Reynolds number, and external turbulence on heat transfer and film cooling effectiveness, ASME Journal of Turbomachinery, 132 (1) (2010) 011017.
J. Choi, S. Mhetras, J. C. Han, S. Lau and R. Rudolph, Film cooling and heat transfer on two cutback trailing edge model with internal performance blockages, Journal of Heat Transfer, 130 (1) (2008) 012201.
Y. Chen, C. G. Matalanis and J. K. Eaton, High resolution PIV measurements around a model turbine blade trailing edge film cooling breakout, Experiments in Fluids, 44 (2) (2008) 199–209.
H. J. Rehder, Investigation of trailing edge cooling concepts in a high pressure turbine cascade: Aerodynamic experiments and loss analysis, ASME Paper No. GT 2009-59303.
A. Dannhauer, Investigation of trailing edge cooling concepts in a high pressure turbine cascade—analysis of the adiabatic film cooling effectiveness, ASME Paper No. GT 2009-59343.
J. Krueckels, M. Gritsch and M. Schnieder, Design consideration and validation of trailing edge pressure side bleed cooling, ASME Paper No. GT 2009-59161.
T. Horbach, A. Schulz and H. J. Bauer, Trailing edge film cooling of gas turbine airfoils-effects of ejection lip geometry on film cooling effectiveness and heat transfer, Heat Transfer Research, 41 (8) (2010) 849–865.
T. Horbach, A. Schulz and H. J. Bauer, Trailing edge film cooling of gas turbine airfoils -external cooling performance of various internal pin fin configurations, ASME Journal of Turbomachinery, 133 (4) (2011) 041006.
A. Murata, S. Nishida, H. Saito, K. Iwamoto, Y. Okita and C. Nakamata, Effects of surface geometry on film cooling performance at airfoil trailing edge, ASME Journal of Turbomachinery, 134 (5) (2012) 051033.
A. Murata, K. Yano, M. Hanai, H. Saito and K. Iwamoto, Arrangement effects of inclined teardrop-shaped dimples on film cooling performance of dimpled cutback surface at airfoil trailing edge, International Journal of Heat and Mass Transfer, 107 (2017) 761–770.
G. Barigozzi, A. Perdichizzi and S. Ravelli, Pressure side and cutback trailing edge film cooling in a linear nozzle vane cascade at different Mach numbers, ASME Journal of Turbomachinery, 134 (5) (2012) 051037.
G. Barigozzi, A. Armellini, C. Mucignat and L. Casarsa, Experimental investigation of the effects of blowing conditions and Mach number on the unsteady behavior of coolant ejection through a trailing edge cutback, International Journal of Heat and Fluid Flow, 37 (2012) 37–50.
J. Ling, C. J. Elkins, M. J. Benson, S. D. Yapa and J. K. Eaton, Measurements of a trailing edge slot film cooling geometry designed for reduced coolant flowrate and high surface effectiveness, ASME Paper No. GT 2013-94292.
J. Ling, C. J. Elkins and J. K. Eaton, The effect of land taper angle on trailing edge slot film cooling, ASME Journal of Turbomachinery, 137 (7) (2015) 071003.
G. Wang, J. Estevadeordal, J. DeLancey, J. Bailey, J. Kopriva and G. Laskowski, Experimental and numerical investigations of the heat transfer and flow field in a trailing edge cooling geometry: Part 1—experimental study with IR thermography and PIV, ASME Paper No. GT 2015-43841.
R. Becchi, B. Facchini, A. Picchi, L. Tarchi, D. Coutandin and S. Zecchi, Film cooling adiabatic effectiveness measurements of pressure side trailing edge cooling configurations, Propulsion and Power Research, 4 (4) (2015) 190–201.
N. Gurram, P. T. Ireland, T. H. Wong and K. P. Self, Study of film cooling in the trailing edge region of a turbine rotor blade in high speed flow using pressure sensitive paint, ASME Paper No. GT 2016-57356.
J. Joo and P. Durbin, Simulation of turbine blade trailing edge cooling, Journal of Fluids Engineering, 131 (2) (2009) 021102.
Y. Egorov, F. R. Menter, R. Lechner and D. Cokljat, The scale-adaptive simulation method for unsteady turbulent flow predictions. Part 2: application to complex flows, Flow, Turbulence and Combustion, 85 (1) (2010) 139–165.
H. Schneider, D. von Terzi and H. J. Baurer, Turbulent heat transfer and large coherent structures in trailing-edge cutback film cooling, Flow, Turbulence and Combustion, 88 (1) (2012) 101–120.
H. Schneider, D. Von Terzi, H. J. Bauer and W. Rodi, Coherent structures in trailing-edge cooling and the challenge for turbulent heat transfer modelling, International Journal of Heat and Fluid Flow, 51 (2015) 110–119.
S. Ravelli and G. Barigozzi. Application of unsteady CFD methods to trailing edge cutback film cooling, ASME Paper No. GT 2014-25435.
E. Ivanova, G. Ledezma, G. Wang and G. M. Laskowski, Experimental and numerical investigations of the heat transfer and flow field in a trailing edge cooling geometry: Part 2 -les and hybrid RANS/LES study, ASME Paper No. GT 2015-43603.
M. Effendy, Y. F. Yao, J. Yao and D. R. Marchant, DES study of blade trailing edge cutback cooling performance with various lip thicknesses, Applied Thermal Engineering, 99 (2016) 434–445.
F. R. Menter, Best practice: Scale-resolving simulations in ANSYS CFD, ANSYS Germany GmbH (2012) 1–70.
P. R. Spalart, W. H Jou, M. Strelets and S. R. Allmaras, Comments on the feasibility of LES for wings, and on a hybrid RANS/LES approach, Advances in DNS/LES, 1 (1997) 4–8.
M. Strelets, Detached eddy simulation of massively separated flows, 39th Aerospace Sciences Meeting and Exhibit (2001) 879.
ANSYS CFX, Release 11.0: ANSYS CFX-Solver theory guide, ANSYS (2006).
C. H. Sieverding and H. Heinemann, The influence of boundary layer state on vortex shedding from flat plates and turbine cascades, ASME Journal of Turbomachinery, 112 (2) (1990) 181–187.
G. L. Brown and A. Roshko, On density effects and large structure in turbulent mixing layers, Journal of Fluid Mechanics, 64 (4) (1974) 775–816.
L. P. Bernal and A. Roshko, Streamwise vortex structure in plane mixing layers, Journal of Fluid Mechanics, 170 (1) (1986) 499–525.
Author information
Authors and Affiliations
Corresponding author
Additional information
Recommended by Associate Editor Seong Hyuk Lee
Yan Gao is a Ph.D. candidate of Institute of Turbomachinery, Xi’an Jiaotong University. His research interests include turbomachinery aerodynamics and film cooling technology of gas turbine.
Xin Yan is a Professor at Institute of Turbomachinery, Xi’an Jiaotong University. His main research interest has been in Computational Fluid Dynamics with emphasis in turbomachinery aerodynamics and heat transfer. He is also involved in experimental work to understand complex flow physics.
Rights and permissions
About this article
Cite this article
Gao, Y., Yan, X., Li, J. et al. Investigations into film cooling and unsteady flow characteristics in a blade trailing-edge cutback region. J Mech Sci Technol 32, 5015–5029 (2018). https://doi.org/10.1007/s12206-018-0949-3
Received:
Revised:
Accepted:
Published:
Issue Date:
DOI: https://doi.org/10.1007/s12206-018-0949-3