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How Thickness and Material Properties Influence Thermal Shock Stresses in Flat Plates and Cylinders PUBLIC ACCESS

[+] Author Affiliations
W. Albrecht

AVCO Lycoming Division, Stratford, CT

Paper No. 69-GT-107, pp. V001T01A076; 12 pages
doi:10.1115/69-GT-107
From:
  • ASME 1969 Gas Turbine Conference and Products Show
  • ASME 1969 Gas Turbine Conference and Products Show
  • Cleveland, Ohio, USA, March 9–13, 1969
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7983-2
  • Copyright © 1969 by ASME

abstract

Thermal stresses in a flat plate, a solid and a hollow cylinder are calculated for sudden changes in ambient temperature using analytical solutions. The sudden temperature change from T1 to T2 is approximated by a step change and a linear change. Use of these approximations allows an evaluation of the actual stresses in close limits.

The analytical solutions for transient temperatures and stresses have been made dimensionless in order to gain general information. Thus it became possible to investigate the effect of geometry and wall thickness of a body, heat transfer characteristics and material properties on thermal shock stresses. Charts for quick evaluation of thermal shock stresses are included.

Copyright © 1969 by ASME
This article is only available in the PDF format.

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