Abstract
This paper presents a proposed approach for improving the design of a composite pressure vessel (CPV) under internal pressure. Thin shell theory, membrane theory, classical lamination theory and Tsai-Wu failure criterion are carefully integrated into an efficient mathematical model. The mathematical model is successfully combined with an in-house developed algorithm that is used to improve the design of any given CPV. Case results show that the proposed approach successfully improved the design of a composite pressure vessel relative to the base design made from steel and also relative to a conventional CPV design approach.
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CITATION STYLE
Mahdy, W., Taher, H., & El-Soaly, E. (2013). Design Improvement of Composite Pressure Vessel Structure. International Conference on Aerospace Sciences and Aviation Technology, 15(AEROSPACE SCIENCES), 1–12. https://doi.org/10.21608/asat.2013.22241
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