An Initial and Progressive Failure Analysis for Cryogenic Composite Fuel Tank Design

Thermal residual stresses, internal pressure stresses, and acceleration stresses during launch were evaluated and quantified for cryogenic composite fuel tank design. Both failure initiation and progression of graphite/epoxy laminate system (IM7/977-2) [0/90/90/0/0/90]s and graphite/BMI laminate sys...

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Veröffentlicht in:	Journal of composite materials 2007-11, Vol.41 (21), p.2545-2568
Hauptverfasser:	Ju, Jaehyung, Pickle, Brent D., Morgan, Roger J., Reddy, J.N.
Format:	Artikel
Sprache:	eng
Schlagworte:	Applied sciences Composites Exact sciences and technology Forms of application and semi-finished materials Fracture mechanics (crack, fatigue, damage...) Fundamental areas of phenomenology (including applications) Physics Polymer industry, paints, wood Solid mechanics Static elasticity (thermoelasticity...) Structural and continuum mechanics Technology of polymers
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