Structural behaviour modelling of bolted joints in composite laminates subjected to cyclic loading-Reference-Cited by-同舟云学术

Structural behaviour modelling of bolted joints in composite laminates subjected to cyclic loading

Published:2015-06 Issue: Volume:43 Page:89-95
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Scarselli G.^ORCID,Castorini E.,Panella F.W.,Nobile R.,Maffezzoli A.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference19 articles.

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2. ASTM D5961. Standard test method for bearing response of polymer-matrix composite laminates, vol. 15.03,2005

3. ASTM D7248. Standard test method for bearing/bypass interaction response of polymer-matrix composite laminates using 2-fastener specimen, vol. 15.03,2007

4. Airfoil structural morphing based on S.M.A. actuator series: numerical and experimental studies;Barbarino;J. Intell. Mater. Syst. Struct.,2011

5. Forced vibration of mechanical systems with hysteresis;Bouc,1967

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