Numerical predictions of augmented heat transfer of an internal blade tip-wall by hemispherical dimples

• Published in: International journal of heat and mass transfer Vol. 53; no. 25; pp. 5639 - 5650
• Main Authors: Xie, Gongnan, Sundén, Bengt
• Format: Journal Article
• Language: English
• Published: Kidlington Elsevier Ltd 01-12-2010; Elsevier
• Subjects: Active area; Applied sciences; Blades; Computation; Computational fluid dynamics; Dimples; Dimpling; Energiteknik; Energy; Energy Engineering; Energy. Thermal use of fuels; Engineering and Technology; Engines and turbines; Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc; Exact sciences and technology; Fluid flow; Heat transfer; Maskinteknik; Mathematical models; Mechanical Engineering; Teknik; Tip-wall; Turbulence; Turbulent flow; Active area; Dimples; Computation; Tip-wall; Heat transfer; Rectangular pipe; Turbulent flow; Boundary condition; Indentation; Modeling; Three dimensional flow; Pressure drop; Cooling system; Turbine blade; Numerical simulation; Gas turbine; Performance
• ISSN: 0017-9310; 1879-2189
• DOI: 10.1016/j.ijheatmasstransfer.2010.08.019

The heat transferred to the turbine blade is substantially increased as the turbine inlet temperature is increased. Improved cooling methods are therefore needed for the turbine blades to ensure a long durability and safe operation. The blade tip region is exposed to very hot gas flow, and suffers high local thermal loads due to the external tip leakage flow. A common way to cool the tip is to design serpentine passages with 180° turn under the blade tip-cap taking advantage of the three-dimensional turning effect and impingement. Increased internal convective cooling is therefore required to increase the blade tip lifetime. In this paper, augmented heat transfer of a blade tip with internal hemispherical dimples has been investigated numerically. The computational models consist of two-pass channels with 180° turn and arrays of dimples depressed on the internal tip-cap. Turbulent convective heat transfer between the fluid and dimples, and heat conduction within dimples and tip are simultaneously computed. The inlet Reynolds number is ranging from 100,000 to 600,000. Details of the 3D fluid flow and heat transfer over the tip-walls are presented. Comparisons of the overall performance of the models are presented. It is found that due to the combination of turning impingement and dimple-induced advection flow, the heat transfer coefficient of the dimpled tip is up to two times higher than that of a smooth tip with less than 5% pressure drop penalty. It is suggested that the use of dimples is suitable for augmenting blade tip cooling to achieve an optimal balance between thermal and mechanical design requirements.