Mechanical integrity of friction-riveted joints for aircraft applications

Author:

Borba N.Z.,Kötter B.,Fiedler B.,dos Santos J.F.,Amancio-Filho S.T.

Funder

CNPq

Helmholtz Association through the Young Investigator Group

Austrian aviation programme TAKE OFF

BMVIT-Austrian Ministry for Transport, Innovation, and Technology

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference41 articles.

1. Airframe Structural Design: Practical Design Information and Data on Aircraft Structures. Hong Kong;Niu,1988

2. 8 – Considerations of failure mechanisms in polymer matrix composites in the design of aerospace structures;Tsotsis,2012

3. Commercial Aircraft Composite;Breuer,2016

4. Static and dynamic failure behaviour of bolted joints in carbon fibre composites;Heimbs;Compos Part Appl Sci Manuf,2013

5. Fatigue crack location and fatigue life for riveted lap joints in aircraft fuselage;Skorupa;Int J Fatigue,2014

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