Effects of transient dynamic loading on the energy absorption capability of composite bolted joints undergoing extended bearing failure

Author:

Feser Thomas,Hassan Jazib,Waimer Matthias,O'Higgins Ronan M.,McCarthy Conor T.,Toso Nathalie,Voggenreiter Heinz,McCarthy Michael A.

Funder

ICONIC

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference27 articles.

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2. FAA. Special Conditions: Boeing Model 787-8 Airplane; Crashworthiness; Docket No. NM368 Special Conditions No. 25-07-05-SC. US Federal Register 2007.

3. Kindervater C, Georgi H. Composite strength and energy absorption as an aspect of structural crash resistance. Structural crashworthiness and failure. 1993:189–235.

4. Contribution to an improved crash design for a composite transport aircraft fuselage—development of a kinematics model and an experimental component test setup;Waimer;CEAS Aeronaut J,2013

5. Composite crash absorber for aircraft fuselage applications;Heimbs;Struct Under Shock Impact,2010

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