Kalyan 4-25-08
Region 3 sector orientations can be understood as follows
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| Figure 4.25.08.1: sector orientation |
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| Figure 4.25.08.2: sector orientation |
5 Analysis were carried out as follows.
All of them with Carbon rods, No Hexcel sheet, No mylar sheet. Left hinge was constrained, right hinge was allowed to move along the back Plate length(x-axis) and front face of the nose plate was constrained.
- Wire Loads are 1512N on all the 4 hole areas
- Material Properties
| Name of the Material | Young's Modulus (MPa) | Density (kg/Cu.mm ) | Poisson's Ratio |
| Polyurethane | 66 | 2.4e-007 | 0.3 |
| Aluminum | 68900 | 2.7e-006 | 0.33 |
| Stainless steel | 1.93e+005 | 8.e-006 | 0.3 |
| Carbon fiber | 1.5e+005 | 5.8e-007 | 0.3 |
Case 1. No gravity
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| Figure 4.25.08.1: Total Deformation in analysis Case 1 |
The remaining pictures with X, Y, Z Deformations are available at Remaining pictures of Case_1
The analysis report is available at File:4 25 08 1.pdf
Case 2. Ideal case of gravity
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| Figure 4.25.08.2: Total Deformation in analysis Case 2 |
The remaining pictures with X, Y, Z Deformations are available at Remaining pictures of Case_2
The analysis report is available at File:4 25 08 2.pdf
Case 3. Chamber 3
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| Figure 4.25.08.3: Total Deformation in analysis Case 3 |
The remaining pictures with X, Y, Z Deformations are available at Remaining pictures of Case_3
The analysis report is available at File:4 25 08 3.pdf
Case 4. Chamber 4
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| Figure 4.25.08.4: Total Deformation in analysis Case 4 |
The remaining pictures with X, Y, Z Deformations are available at Remaining pictures of Case_4
The analysis report is available at File:4 25 08 4.pdf
Case 5. Chamber 5
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| Figure 4.25.08.5: Total Deformation in analysis Case 5 |
The remaining pictures with X, Y, Z Deformations are available at Remaining pictures of Case_5
The analysis report is available at File:4 25 08 5.pdf