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


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.

National Technical University of Athens

Read the Original

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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