This paper presents a novel experimental technique, which combines thermochromic liquid crystals with multiple steps in gas temperature, to determine heat transfer coefficient and adiabatic wall temperature distributions. The transient heat transfer experiments have been conducted on a flat plate using the low-temperature analogue of an ISO standard propane-air burner commonly used in aero-engine fire certification. The technique involves the measurement of the surface temperature response of an insulating model to a change in gas temperature. A coating comprising more than one thermochromic liquid crystal material is used to increase the range of the surface measurement and this is combined with multiple step changes in gas temperature. These measures induce several peaks in liquid crystal intensity throughout the transient experiment and these are shown to improve the accuracy. The current technique employs useful data from both the heating and cooling phases in the heat transfer test. To the authors’ knowledge, this has not been investigated before and it is likely to be very useful for other applications of the liquid crystal transient heat transfer experiment. The uncertainties in all measurements have been quantified and are presented in this paper.
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October 2004
Technical Papers
A Novel Liquid Crystal Image Processing Technique Using Multiple Gas Temperature Steps to Determine Heat Transfer Coefficient Distribution and Adiabatic Wall Temperature
Abd Rahim Abu Talib,
Abd Rahim Abu Talib
Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, Serdang, 43400 Selangor, Malaysia
11
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Andrew J. Neely,
Andrew J. Neely
School of Aerospace and Mechanical Engineering, University of New South Wales, Australian Defense Force Academy, Northcott Drive, Canberra ACT 2600, Australia
11
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Peter T. Ireland,
Peter T. Ireland
Department of Engineering Science, University of Oxford, Parks Road, Oxford OX1 3PJ, UK
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Andrew J. Mullender
Andrew J. Mullender
Fire Precautions Group, Rolls-Royce plc., P.O. Box 31, Derby DE24 8BJ, UK
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Abd Rahim Abu Talib
11
Department of Aerospace Engineering, Faculty of Engineering, Universiti Putra Malaysia, Serdang, 43400 Selangor, Malaysia
Andrew J. Neely
11
School of Aerospace and Mechanical Engineering, University of New South Wales, Australian Defense Force Academy, Northcott Drive, Canberra ACT 2600, Australia
Peter T. Ireland
Department of Engineering Science, University of Oxford, Parks Road, Oxford OX1 3PJ, UK
Andrew J. Mullender
Fire Precautions Group, Rolls-Royce plc., P.O. Box 31, Derby DE24 8BJ, UK
Contributed by the International Gas Turbine Institute and presented at the International Gas Turbine and Aeroengine Congress and Exhibition, Atlanta, GA, June 16–19, 2003. Manuscript received by the IGTI December 2002; final revision March 2003. Paper No. 2003-GT-38198. Review Chair: H. R. Simmons.
J. Turbomach. Oct 2004, 126(4): 587-596 (10 pages)
Published Online: December 29, 2004
Article history
Received:
December 1, 2002
Revised:
March 1, 2003
Online:
December 29, 2004
Citation
Talib, A. R. A., Neely, A. J., Ireland, P. T., and Mullender, A. J. (December 29, 2004). "A Novel Liquid Crystal Image Processing Technique Using Multiple Gas Temperature Steps to Determine Heat Transfer Coefficient Distribution and Adiabatic Wall Temperature ." ASME. J. Turbomach. October 2004; 126(4): 587–596. https://doi.org/10.1115/1.1776585
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