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Adhesively Bonded Composite Structures: Process Control, Non Destructive Inspection, and Strength Effects
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English
Abstract
Quality, inspectability, and strength of adhesively bonded joints is discussed. Lap shear specimens with flaws possible during manufacture of bonded joints were fabricated and tested. Flaw included contamination and improper processing. Severity of the flaws was ranked by reduction in strength. The content of an on-going program to correlate non-destructive inspection response with strength significant flaws is suggested.
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Authors
Citation
Wong, R., "Adhesively Bonded Composite Structures: Process Control, Non Destructive Inspection, and Strength Effects," SAE Technical Paper 891044, 1989, https://doi.org/10.4271/891044.Also In
References
- SAE paper 871022 “Certification of Bonded Composite Structure” Jonas Paul Aldag Tom Beech Aircraft Corp
- “Transcripts of the Presentations at the Workshop on NDE of Adhesive Bond Strength” April 13-14 1988 Orlando, Florida
- “Design, Fabrication, and Certification of the All-Composite Airframe” Abbott Ric to be published at SAE Aerotech Conference 1989