A Numerical study of fluid flow, heat transfer and pressure drop in a stationary matrix cooling channel having an angle of 45 degrees for the three Reynolds numbers (24000<Re<60000) and four sub-channel aspect ratios (0.5<W/H<1.2) have been performed. This includes different shaped sub-channels such as Rectangular, U, and then two, three layered matrix combined with open and closed matrix channels. The simulation shows the development of vortices along the channel. The flow turning and impingement after hitting the side wall have significant contribution to the heat transfer enhancement. The Nusselt number and friction factor have been evaluated and compared with limited experimental results. The highest heat transfer enhancement is found at impingement region as the flow takes turn and impinges on to the wall. But slight enhancement in heat transfer is observed at turning region. The sub-channel aspect ratio has less impact on heat transfer enhancement, but more effect on pressure drop. The performance of closed matrix is relatively better than the open matrix one. The overall thermal performance (η) of the matrix having U sub-channel is nearly 10% higher than the rectangular sub-channel.
Skip Nav Destination
ASME 2014 Gas Turbine India Conference
December 15–17, 2014
New Delhi, India
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-4964-4
PROCEEDINGS PAPER
Computational Study of Flow and Heat Transfer in Matrix Cooling Channels
Sivasankara Reddy Ramireddy,
Sivasankara Reddy Ramireddy
Gas Turbine Research Establishment, Bangalore, India
Search for other works by this author on:
Siddappa Pallavagere Gurusiddappa,
Siddappa Pallavagere Gurusiddappa
Siddaganga Institute of Technology, Tumkur, India
Search for other works by this author on:
V. Kesavan,
V. Kesavan
Gas Turbine Research Establishment, Bangalore, India
Search for other works by this author on:
S. Kishore Kumar
S. Kishore Kumar
Gas Turbine Research Establishment, Bangalore, India
Search for other works by this author on:
Sivasankara Reddy Ramireddy
Gas Turbine Research Establishment, Bangalore, India
Siddappa Pallavagere Gurusiddappa
Siddaganga Institute of Technology, Tumkur, India
V. Kesavan
Gas Turbine Research Establishment, Bangalore, India
S. Kishore Kumar
Gas Turbine Research Establishment, Bangalore, India
Paper No:
GTINDIA2014-8252, V001T04A007; 7 pages
Published Online:
February 19, 2015
Citation
Ramireddy, SR, Gurusiddappa, SP, Kesavan, V, & Kumar, SK. "Computational Study of Flow and Heat Transfer in Matrix Cooling Channels." Proceedings of the ASME 2014 Gas Turbine India Conference. ASME 2014 Gas Turbine India Conference. New Delhi, India. December 15–17, 2014. V001T04A007. ASME. https://doi.org/10.1115/GTINDIA2014-8252
Download citation file:
58
Views
Related Proceedings Papers
Related Articles
Latticework (Vortex) Cooling Effectiveness: Rotating Channel Experiments
J. Turbomach (July,2005)
Numerical and Experimental Study on the Heat Transfer and Pressure Drop of Compact Cross-Corrugated Recuperators
J. Heat Transfer (July,2014)
Microchannels With Manufacturing Roughness Levels
J. Turbomach (October,2011)
Related Chapters
Hydraulic Resistance
Heat Transfer & Hydraulic Resistance at Supercritical Pressures in Power Engineering Applications
Adding Surface While Minimizing Downtime
Heat Exchanger Engineering Techniques
The Design and Implement of Remote Inclinometer for Power Towers Based on MXA2500G/GSM
International Conference on Mechanical and Electrical Technology, 3rd, (ICMET-China 2011), Volumes 1–3