When the operating condition of a gas turbine engine changes from one steady-state to another, the cooling must ensure that the solid's temperatures never exceed the maximum allowable throughout the transient process. Exceeding the maximum allowable temperature is possible even though cooling is increased to compensate for the increase in heating because there is a time lag in how the solid responds to changes in its convective heating and cooling environments. In this paper, a closed-form solution (referred to as the 1D model) is derived to estimate the over temperature and its duration in a flat plate subjected to sudden changes in heating and cooling rates. For a given change in heating rate, the 1D model can also be used to estimate the minimum cooling needed to ensure that the new steady-state temperature will not exceed the maximum allowable. In addition, this model can estimate the temperature the material must be cooled to before imposing a sudden increase in heat load to ensure no over temperature throughout the transient process. Comparisons with the exact solutions show the 1D model to be accurate within 0.1%. This 1D model was generalized for application to problems in multidimensions. The generalized model was used to estimate the duration of over temperature in a two-dimensional problem involving variable heat transfer coefficient (HTC) on the cooled side of a flat plate and provided results that match the exact solution within 5%.
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June 2016
Research-Article
Estimating Over Temperature and Its Duration in a Flat Plate With Sudden Changes in Heating and Cooling
Chien-Shing Lee,
Chien-Shing Lee
School of Aeronautics and Astronautics,
Purdue University,
West Lafayette, IN 47907-2045
e-mail: cslee@purdue.edu
Purdue University,
West Lafayette, IN 47907-2045
e-mail: cslee@purdue.edu
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Tom I-P. Shih,
Tom I-P. Shih
School of Aeronautics and Astronautics,
Purdue University,
West Lafayette, IN 47907-2045
e-mail: tomshih@purdue.edu
Purdue University,
West Lafayette, IN 47907-2045
e-mail: tomshih@purdue.edu
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Kenneth Mark Bryden
Kenneth Mark Bryden
Department of Mechanical Engineering,
Iowa State University,
Ames, IA 50011
e-mail: kmbryden@iastate.edu
Iowa State University,
Ames, IA 50011
e-mail: kmbryden@iastate.edu
Search for other works by this author on:
Chien-Shing Lee
School of Aeronautics and Astronautics,
Purdue University,
West Lafayette, IN 47907-2045
e-mail: cslee@purdue.edu
Purdue University,
West Lafayette, IN 47907-2045
e-mail: cslee@purdue.edu
Tom I-P. Shih
School of Aeronautics and Astronautics,
Purdue University,
West Lafayette, IN 47907-2045
e-mail: tomshih@purdue.edu
Purdue University,
West Lafayette, IN 47907-2045
e-mail: tomshih@purdue.edu
Kenneth Mark Bryden
Department of Mechanical Engineering,
Iowa State University,
Ames, IA 50011
e-mail: kmbryden@iastate.edu
Iowa State University,
Ames, IA 50011
e-mail: kmbryden@iastate.edu
1Corresponding author.
Contributed by the International Gas Turbine Institute (IGTI) of ASME for publication in the JOURNAL OF TURBOMACHINERY. Manuscript received December 3, 2015; final manuscript received December 9, 2015; published online February 9, 2016. Editor: Kenneth C. Hall.
J. Turbomach. Jun 2016, 138(6): 061007 (12 pages)
Published Online: February 9, 2016
Article history
Received:
December 3, 2015
Revised:
December 9, 2015
Citation
Lee, C., Shih, T. I., and Mark Bryden, K. (February 9, 2016). "Estimating Over Temperature and Its Duration in a Flat Plate With Sudden Changes in Heating and Cooling." ASME. J. Turbomach. June 2016; 138(6): 061007. https://doi.org/10.1115/1.4032306
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