Spring-back of Thick Uni-Directional Carbon Fibre Reinforced Composite Laminate for Aircraft Structure Application

• Published in: Journal of physics. Conference series Vol. 1005; no. 1; pp. 12003 - 12009
• Main Authors: Zakaria, M, Aminanda, Y, Rashidi, S A, Sah, M A Mat
• Format: Journal Article
• Language: English
• Published: Bristol IOP Publishing 01.04.2018
• Subjects: Aerospace industry; Aircraft; Aircraft structures; Carbon fibers; Fiber composites; Lay-up; Micrometers; Optical scanners; Physics; Production methods; Springback

The springback phenomena of CFRP after curing process through autoclave manufacturing method results on the out of tolerance for its utilisation in aerospace industry. This paper relates to the measurements of springback for Uni-directional flat laminate as a first steps to the springback study for...