Show transcribed image text A unidirectional lamina specimen made of AS/3501 carbon/epow to an off-axis tensile test with θ=45° as shown in Figure 4.SUiyls subjected mum stress criterion, determine (a) the value of the applied st be required to produce longitudinal tensile failure, (b) the val PROBLEM 4.1 sing the stress o, that would of the applied (c) the value tensie max, hear stress o, that would be required to produce in-plane shear failure,e ofthe applied stress σ, that would be required to produce trans failure, and (d) which of the failure modes described in parts (a), Gh would actually cause failure of the specimen, and why PROBLEM 4.2 the applied stress a, is compressive in Problem 4.1, use the ma maximun would stress criterion to determine (a) the value of the applied stress o, that be required to produce longitudinal compressive failure, (b) the value applied stress o, that would be required to produce in-plane shear failure ( the value of the applied stress o, that would be required to produce trans verse compressive failure, and (d) which of the failure modes described in parts (a) (b), and (c) would actually cause failure of the specimen, and why
A unidirectional lamina specimen made of AS/3501 carbon/epow to an off-axis tensile test with θ=45° as shown in Figure 4.SUiyls subjected mum stress criterion, determine (a) the value of the applied st be required to produce longitudinal tensile failure, (b) the val PROBLEM 4.1 sing the stress o, that would of the applied (c) the value tensie max, hear stress o, that would be required to produce in-plane shear failure,e ofthe applied stress σ, that would be required to produce trans failure, and (d) which of the failure modes described in parts (a), Gh would actually cause failure of the specimen, and why PROBLEM 4.2 the applied stress a, is compressive in Problem 4.1, use the ma maximun would stress criterion to determine (a) the value of the applied stress o, that be required to produce longitudinal compressive failure, (b) the value applied stress o, that would be required to produce in-plane shear failure ( the value of the applied stress o, that would be required to produce trans verse compressive failure, and (d) which of the failure modes described in parts (a) (b), and (c) would actually cause failure of the specimen, and why





