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Design of a composite tube to analyze the compressive behavior of CFRP
Affiliation:1. Laboratoire de Mécanique et d’Acoustique, CNRS – UPR 7051, 31 chemin Joseph Aiguier, 13402 Marseille Cedex 20, France;2. Centre de Recherche de l’Armée de l’Air, CReA 10.401, B.A. 701, 13661 Salon-Air, France;3. Aix Marseille Université, 60 Rue Frédéric Joliot Curie, 13013 Marseille, France;1. Department of Engineering Thermophysics, School of Energy and Power Engineering, Beihang University, Beijing 100191, China;2. Department of Aircraft Airworthiness Engineering, School of Transportation Science and Engineering, Beihang University, Beijing 100191, China;3. Aircraft/Engine Integrated System Safety Beijing Key Laboratory, Beijing 100191, China;4. AVIC Shaanxi QianShan Avonics co., Ltd., Xi’an 710065, China;1. Institute of Structural Analysis, Leibniz Universität Hannover, Germany;2. LMT-Cachan (ENS Cachan/CNRS/Université Paris-Saclay), F-94230 Cachan, France;1. Qatar University, Department of Chemical Engineering, College of Engineering, Doha, PO. Box-2713, Qatar;2. Qatar University, Department of Mechanical and Industrial Engineering, College of Engineering, Doha, PO. Box-2713, Qatar
Abstract:A dumbbell-shaped tube is designed in order to study the compression of composites in the direction of the fibers. Three conditions are defined that ensure the validity of the experimental procedure: the cracks appear in the middle of the specimen, the strain field is homogeneous in the gauge area, and buckling must be avoided. Several tubes are manufactured and then analyzed to verify that they satisfy these three conditions. It turns out that a [0°]11 woven carbon/epoxy (G939/M18) tube reinforced with [90°] unbalanced woven glass/epoxy tabs (1055/ES18) is suitable for compression tests.The non linear elastic behavior of the material is then identified. The values of the parameters are close to those identified in a pure bending test.
Keywords:Compression  Experimental  Composites  Buckling  Tube  Dumbbell-shaped
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