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A Model for Analyzing Cracking of Coatings

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Lempriere, Brian M., author.
Conference Name:
Airframe Finishing, Maintenance & Repair Conference & Exposition (1995-03-13 : Seattle, Washington, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1995
Summary:
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
Notes:
Vendor supplied data
Publisher Number:
951137
Access Restriction:
Restricted for use by site license

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