What is it about?

The significance in the external to internal loading reduction when using fibrous polymer composite materials in the airframe industry

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Why is it important?

The area under investigation, the joint between the fuselage and the pressure bulkhead, is a critical location, the sizing of which in the case of fibre composite laminates has to be dealt with in greater detail

Perspectives

Writing this article was a great pleasure as it has co-authors with whom I have had long-standing collaborations. This article also lead to rare disease groups contacting me and ultimately to greater involvement in rare disease research.

Professor EFSTATHIOS E. THEOTOKOGLOU
National Technical University of Athens

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This page is a summary of: Design and Numerical Modeling of a Pressurized Airframe Bulkhead Joint, Journal of Aircraft, November 2015, American Institute of Aeronautics and Astronautics (AIAA), DOI: 10.2514/1.c033473.
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Contributors

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