What is it about?
The significance in the external to internal loading reduction when using fibrous polymer composite materials in the airframe industry
Featured Image
Photo by Drew Beamer on Unsplash
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
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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Contributors
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