Difference between revisions of "Kalyan 4-25-08"
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{| border="1" |cellpadding="20" cellspacing="0 | {| border="1" |cellpadding="20" cellspacing="0 | ||
|- | |- | ||
− | |Name of the Material|| Young's Modulus (MPa) || Density ( ) || Poisson's Ratio | + | |Name of the Material|| Young's Modulus (MPa) || Density (kg/Cu.mm ) || Poisson's Ratio |
|- | |- | ||
− | | Polyurethane || | + | | Polyurethane || 66 || 2.4e-007 || 0.3 |
|- | |- | ||
− | | Aluminum | + | | Aluminum || 68900 || 2.7e-006 || 0.33 |
|- | |- | ||
− | | stainless steel || | + | | stainless steel || 1.93e+005|| 8.e-006 || 0.3 |
|- | |- | ||
| Carbon fiber || 4/14/08|| 9/22/08 || 9/22/08 | | Carbon fiber || 4/14/08|| 9/22/08 || 9/22/08 |
Revision as of 22:13, 25 April 2008
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 | 4/14/08 | 9/22/08 | 9/22/08 |
Case 1. No gravity
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
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
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
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
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