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Advances in Aircraft and Spacecraft Science   Volume 6, Number 1, January 2019, pages 069-86
DOI: http://dx.doi.org/10.12989/aas.2019.6.1.069
 
Full field strain measurements of composite wing by digital image correlation
A. Pagani, E. Zappino, A.G. de Miguel, V. Martilla and E. Carrera

 
Abstract     [Full Text]
    This paper discusses the use of the Digital Image Correlation (DIC) technique for the displacement and strain measurements of a wet lay-up composite wing. As opposed to classical strain gages, DIC allows to conduct full field strain analysis of simple to complex structural parts. In this work, wing-up bending tests and measurements of the composite wing of the Dardo Aspect by CFM Air are carried out through an ad-hoc test rig and the Q-400 DIC system by Dantec Dynamics. Also, the results are used to validate a finite element model of the structure under investigation.
 
Key Words
    digital image correlation; composite wings; full field strain analysis
 
Address
A. Pagani, E. Zappino, A.G. de Miguel and E. Carrera: MUL2 group, Department of Mechanical and Aerospace Engineering, Politecnico di Torino, Turin, Italy
V. Martilla: C.F.M. Air s.r.l., Cirié, Turin, Italy
 

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