Pin fin or full cross pin cooling configurations have long been of interest to the turbine cooling designer because of their potentially high heat transfer characteristics and high surface area density, as well as their structural and castability advantages. The pin fin cooling configurations consist of flow channels with circular pins extending from the walls into the channel flow. The pin fins function as turbulators to produce high heat transfer rate; however, their geometric arrangement must be optimized to avoid high friction loss. Experimental tests have been conducted to investigate the effects of pin heights, spacings, and channel height to length ratios to the heat transfer and friction loss characteristics of the pin fin cooling configurations. The test results indicate that the pin fin configuration provides a means to reduce the flow friction loss and yet to maintain a reasonably high heat transfer rate as compared to the cross pin configuration. The pin spacing in the test range shows less effects on the pin fin performance than the pin height.
Skip Nav Destination
Article navigation
January 1984
Research Papers
Heat Transfer and Friction Loss Characteristics of Pin Fin Cooling Configurations
Yao Peng
Yao Peng
Avco Lycoming Division, Stratford, Conn. 06497
Search for other works by this author on:
Yao Peng
Avco Lycoming Division, Stratford, Conn. 06497
J. Eng. Gas Turbines Power. Jan 1984, 106(1): 246-251 (6 pages)
Published Online: January 1, 1984
Article history
Received:
December 27, 1982
Online:
October 15, 2009
Citation
Peng, Y. (January 1, 1984). "Heat Transfer and Friction Loss Characteristics of Pin Fin Cooling Configurations." ASME. J. Eng. Gas Turbines Power. January 1984; 106(1): 246–251. https://doi.org/10.1115/1.3239544
Download citation file:
Get Email Alerts
Accelerating Chemical Kinetics Calculations with Physics Informed Neural Networks
J. Eng. Gas Turbines Power
Fully Coupled Analysis of Flutter Induced Limit Cycles: Frequency Versus Time Domain Methods
J. Eng. Gas Turbines Power (July 2023)
Impact of Ignition Assistant on Combustion of Cetane 30 and 35 Jet-Fuel Blends in a Compression-Ignition Engine at Moderate Load and Speed
J. Eng. Gas Turbines Power (July 2023)
Related Articles
Cooling Performance of Additively Manufactured Pin Fins in Stacked Microchannels for the Inside-Out Ceramic Turbine Shroud-Cooling Ring
J. Turbomach (July,2022)
The Augmentation of Internal Blade Tip-Cap Cooling by Arrays of Shaped Pins
J. Turbomach (October,2008)
Effect of Pin Density on Heat-Mass Transfer and Fluid Flow at Low Reynolds Numbers in Minichannels
J. Heat Transfer (June,2010)
Identifying Inefficiencies in Unsteady Pin Fin Heat Transfer Using Orthogonal Decomposition
J. Heat Transfer (February,2012)
Related Chapters
Control and Operational Performance
Closed-Cycle Gas Turbines: Operating Experience and Future Potential
Generation of Design Data – Finite Volume Analysis
Compact Heat Exchangers: Analysis, Design and Optimization using FEM and CFD Approach
Exchangers with Longitudinal-Fin Tubes
Heat Exchanger Engineering Techniques