JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
Articles
Contribution of Reduction Method for Energy Release Rate of Adhesive Bonding Structure in Composite Tank around Mouthpiece
Shinsuke TAKEUCHIEiichi SATOJunjiro ONODAYoji ARAKAWAAkira MIYAHARA
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2010 Volume 58 Issue 681 Pages 302-307

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Abstract

This paper includes evaluations of composite tanks or pressure vessels based on fracture mechanics and an improved method for tank design. Problems of exfoliation between the mouthpiece and composite in current composite pressure vessels are shown, and the simple solution by inducing a slit into the mouthpiece near the bonding interface is proposed. The effect of the slit is evaluated using a geometrically simple model as well as a pressure vessel model designed for a rocket.

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© 2010 The Japan Society for Aeronautical and Space Sciences
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