Heat Transfer in a Rib Turbulated Pin Fin Array for Trailing Edge Cooling

Author:

Otto Marcel1,Kapat Jayanta1,Ricklick Mark2,Mhetras Shantanu3

Affiliation:

1. Center for Advanced Turbomachinery and Energy Research, Department of Mechanical and Aeronautical Engineering, University of Central Florida, 12760 Pegasus Drive, Orlando, FL 32816

2. Embry-Riddle Aeronautical University, 1 Aerospace Boulevard, Daytona Beach, FL 32114

3. Siemens Energy Inc., 5101 Westinghouse Boulevard, Charlotte, NC 28273

Abstract

Abstract Ribs were added into a pin fin array for a uniquely new cooling concept enabled through additive manufacturing. Heat transfer measurements are obtained using the thermochromic liquid crystal technique in a trapezoidal duct with pin fins and rib turbulators. Three pin blockage ratios and four rib heights at Reynolds numbers between 40,000 and 106,000 were tested. The Nusselt number augmentation is generally higher at the longer base of the trapezoidal duct. The same high heat transfer trend is seen at the columns closer to the longer base of the trapezoidal duct than on the shorter base. Through the length of the duct, the flow shifts from the nose region to the larger opening on the opposite wall. Also, it is observed that increasing the blockage ratio as well as increasing the rib height has a positive impact on heat transfer as ribs act as additional extended surfaces and alter the near-wall flow field. The heat transfer augmentation of pins and ribs is found to not be equal to the sum of both: Both heat transfer mechanisms are highly non-linear, thus cannot be superimposed. The observed heat transfer augmentation of the combined cases exceeded over the rib and pin only cases by up to 100%, but the weighted friction factor also doubled. The combination of ribs and pins is an excellent concept to achieve more uniform cooling over an array at higher levels when pressure drop is not of concern.

Publisher

ASME International

Subject

Fluid Flow and Transfer Processes,General Engineering,Condensed Matter Physics,General Materials Science

Reference27 articles.

1. Ahmed, L. , 2018, “Detailed Understanding of Flow, Heat Transfer, and Pressure Drop Behavior in a Square Channel With 45 Deg Ribs,” Ph.D. dissertation, University of Central Florida, Orlando, FL.

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3. Developing Heat-Transfer in Rectangular Channels With Rib Turbulators;Han;Int. J. Heat Mass Transfer,1988

4. Heat-Transfer Enhancement in Channels With Turbulence Promoters;Han;J. Eng. Gas Turbines Power,1985

5. Heat Transfer and Pressure Drop Measurements for a Square Channel With 45deg Round-Edged Ribs at High Reynolds Numbers;Rallabandi;ASME J. Turbomach.,2011

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