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Design and Certification of the All-Composite Airframe
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English
Abstract
Examples of the design concepts employed in the Beech Starship all-composite airframe are given; and the methods of material and structural cetification, including damage tolerance and adhesively bonded structures, are discussed.
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Citation
Abbott, R., "Design and Certification of the All-Composite Airframe," SAE Technical Paper 892210, 1989, https://doi.org/10.4271/892210.Also In
References
- FAA Advisory Circular AC 20-107A April 1984
- Environmental Sensitivity of Advanced Composites April 1977
- Abbott Ric Kolarik Ann Strength Substantiation of the All-Composite Airframe SAMPE 33rd International Symposium May 1989
- Jonas Paul Aldag Tom Certification of Bonded Composite Structure SAE paper 871022 April 1987
- Wong Richard Adhesively Bonded Composite Structure SAE paper 891044 April 1989