A Model for Analyzing Cracking of Coatings
951137
03/01/1995
- Event
- Content
- 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.
- Pages
- 9
- Citation
- Lempriere, B., "A Model for Analyzing Cracking of Coatings," SAE Technical Paper 951137, 1995, https://doi.org/10.4271/951137.