A Model for Analyzing Cracking of Coatings

Paper #:
  • 951137

Published:
  • 1995-03-01
Citation:
Lempriere, B., "A Model for Analyzing Cracking of Coatings," SAE Technical Paper 951137, 1995, https://doi.org/10.4271/951137.
Author(s):
Pages:
9
Abstract:
A method for analyzing cracking in the finish coatings on aircraft composite parts is described. The method is based on a model in which cracking is caused by hygrothermal tensile strain induced by cold and dry conditions, enhanced by creep relaxation of hygrothermal compressive stress from hot wet conditions.
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