Certification for Effect of Environment on Composite Properties

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Abstract:

The environment which can have a great effect on the composite aircraft structure performances must be considered during the design and certification process. In this paper, the extreme temperature and humidity span of the worst environment conditions in aircraft structure design and certification are investigated, and some test methods involving environment influences are also discussed. The studying results can be used in design and certification for environment influences of composite aircraft structures.

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Periodical:

Advanced Materials Research (Volumes 284-286)

Pages:

396-400

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Online since:

July 2011

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© 2011 Trans Tech Publications Ltd. All Rights Reserved

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[1] Fawcentt A, Trostle J, Ward S. 777 empennage certification approach, ICCM-11 [R]. Australia: Boeing Commercial Airplane Group, 1997.

Google Scholar

[2] McCarty J E, Johnson R W, Wilson D R. 737 graphite-epoxy horizontal stabilizer certification [C]// Structures, structural dynamics and materials conference, 23rd. New Orleans, 1982.

DOI: 10.2514/6.1982-745

Google Scholar

[3] Jean Rouchon. Certification of composite aircraft structures: achievements and challenges[C]//The 1st International Symposium on Aircraft Airworthiness. Beijing, 2009.

Google Scholar

[4] J W BRISTOW. C42/86 Airworthiness of composite structures-some experiences from civil certification.

Google Scholar

[5] John S. Tomblin, Yeow C. Ng, K. Suresh Raju. Material Qualification and Equivalency for Polymer Matrix Composite Material Systems Updated Procedure, DOT/FAA/AR-03/19, 2003.

Google Scholar

[6] Jean Rouchon. Certification of Aircraft Composite Structures [R]. 2007.

Google Scholar

[7] Department of Defense. MIL-HDBK-17-3F Composite Materials Handbook Volume 1. Polymer Matrix Composite Guidelines for Characterization of Structural Materials [S]. 2002.

DOI: 10.1201/9781482279054-59

Google Scholar

[8] Kan H P, Cordero R, Whitehead R S. Advanced certification methodology for composite structures [R]. DOT/FAA/-96/111, 1997.

Google Scholar

[9] Hans-Jurgen Schmidt, Bianka Schmidt-Brandecker. Fatigue and Damage Tolerance [R]. 2010.

Google Scholar

[10] Kan H P. Assessment of probabilistic certification methodology for composite Structures [R]. DOT/FAA/AR-00/74, 2001.

Google Scholar