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Table 2. 6 in published literature [8] and [9]. Mesh sensitivity analysis using Shell 99 Mesh sensitivity analysis was essential, in order to save computational time without affecting the solution. In analysis using ANSYS software, 10 rigid regions were used which were equally spaced along beam. The permissible values of Edge Sizes are 1, 2, 3, 4, 5, 6, 10, 12, 15, 20, 30 and 60. Graph of mesh sensitivity analysis has been shown in Fig. 5. It is obvious that solution has converged. Results and Discussion According to Ref.

3 2 ρ= 3 1+ 2 1− (22) Fig. 5. Specimen under pure mode I loading condition (DCB test specimen) Fig. 6. Specimen under pure mode II loading condition (ENF test specimen) Fig. 7. Specimen under mixed-mode loading condition (MMB test specimen) Table 3. 01 n = 0 . 5 Y O = 0 . 5 Y c = 0 . 26 ± 0 . 01 k 03 = 9 . 5 YO = 0 . Y c = 0 . 26 ± 0 . 01 k 01 = 2 . m − 2 MPa/ mm γ 1 = 0 . 023 n = 0 . 5 Y O = 0 . m − 2 Y c = 0 . 26 ± 0 . m − 2 k 03 = 9 . 3 × 10 3 = 2 . 4 × 10 3 k 1 0 MPa/ mm MPa/ mm γ 1 = 0 . 25 α = 2 .

01 k 03 = 9 . 5 YO = 0 . Y c = 0 . 26 ± 0 . 01 k 01 = 2 . m − 2 MPa/ mm γ 1 = 0 . 023 n = 0 . 5 Y O = 0 . m − 2 Y c = 0 . 26 ± 0 . m − 2 k 03 = 9 . 3 × 10 3 = 2 . 4 × 10 3 k 1 0 MPa/ mm MPa/ mm γ 1 = 0 . 25 α = 2 . 0 × 1 0 − 2 Arshad Munir and Zaffar M. Khan 47 The energy release rate for pure mode I [20]: M2 GI = (23) bEI Where the width of the specimen is b , E is the longitudinal flexural Young’s modulus and I is the second moment of area of the specimen’s arm. The energy release rate for pure mode II [20]: 3 M2 4 bEI In which, M = cP / 2 , see Figure 6.

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Advanced Materials for Applied Science and Technology by Edited by Arshad Munir Zaffar M. Khan


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