Composite Materials: Testing and Design 1969
DOI: 10.1520/stp49808s
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A Simplified Method of Determining the Inplane Shear Stress-Strain Response of Unidirectional Composites

Abstract: A simple and relatively inexpensive technique is presented for determining the inplane shear stress-strain response of unidirectional composites. The method utilizes the stress-strain results from an uniaxial test on a ±45-deg laminate which is symmetrically laminated about the midplane. Through the use of relations derived from laminated plate theory, expressions are presented which allow the inplane laminae shear stress-strain curve to be incrementally reproduced from the ±45-deg laminate stress-strain curve… Show more

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Cited by 44 publications
(21 citation statements)
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“…Simultaneous recording of the applied load and the strain enables one to determine the shear stress-strain relationship of the specimen. Tensile test on a t4S0 symmetric laminate for determining the in-plane properties of the FRPC was first proposed by Petit (1969). The method was later improved by Rosen (1972).…”
Section: Tensile Test On 145' Symmetric Laminate (Astm D3518-94)mentioning
confidence: 99%
“…Simultaneous recording of the applied load and the strain enables one to determine the shear stress-strain relationship of the specimen. Tensile test on a t4S0 symmetric laminate for determining the in-plane properties of the FRPC was first proposed by Petit (1969). The method was later improved by Rosen (1972).…”
Section: Tensile Test On 145' Symmetric Laminate (Astm D3518-94)mentioning
confidence: 99%
“…Hence, the relative displacement, W M rel , due to bending-twisting of any point located in the load application line, 1 2 , y 0 , to the middle point of the specimen, 1 2 , 1 2 , is derived:…”
Section: Displacement Eld For the Load Application Linementioning
confidence: 99%
“…1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 The displacement of the middle point of the specimen, 1 2 , 1 2 , is…”
Section: Verication Of the Load Application Cylinder Line Displacementmentioning
confidence: 99%
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