Issue 24
A. V. Babushkin et alii, Frattura ed Integrità Strutturale, 24 (2013) 89-95; DOI: 10.3221/IGF-ESIS.24.09 93 For defying elastic modulus at three point bending of laminate composite material should be used refined dependencies, which consider influence of shear deformations and binding maximum flexure max of the beam in the middle of brackets with applied force P, true elastic modulus at bending t f E and interlayer shear modulus G : 2 3 max 1 48 f i k f i E P l h E I l G (1) where k – coefficient, which depends on cross section form of the beam (for rectangular 1.2 k ); 3 12 bh I – moment of inertia of beam cross section. True elastic modulus at bending t f E is bonded with fictitious modulus 3 max 48 i f P l E I in the following ratio 2 1 1 1.2 t f f i h E E G l (2) The higher ratio of thickness of the specimen to its length i h l and the higher degree of anisotropy of composite material, characterized by t f E G , the more different true elastic modulus from fictitious. With one test it is impossible to calculate elastic modulus by formula (1) as it has two unknowns f E and G . So for their determination are tested several specimens with different ratios i h l and then was diagram made, where on the horizontal axis was put off value 2 i h l and on the vertical axis – 1 f E . In this coordinates, relation (2) has to be represented as a straight line, which crosses the vertical axis at the point 1 t f E and slope of this line to the horizontal axis equal 1.2 G . Then value of t f E and G are determined by method of least square. D ISCUSSION OF RESULTS ension test results of highly filled fiberglass specimens (Direct "E" roving 0.7 - orthophthalic polyester resin 0.3) are in the Tab. 1. Temperature, °C Tensile strength at break b MPa Young's modulus in tension E, GPa -30 922.1 34.2 0 980.2 36.8 +22 987.1 47.8 +40 690.5 38.8 +50 - 37.4 Table 1 : Unidirectional fiberglass (Direct "E" roving 0.7 - orthophthalic polyester resin 0.3) properties at tension test [3]. T
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