K 4-25-08

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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

Case 1. No gravity

4 25 08 1d.jpg
Figure 4.25.08.1: Total Deformation in analysis Case 1


The remaining pictures with X, Y, Z Deformations are available atRemaining pictures of Case_1 The analysis report is available at File:4 25 08 1.pdf


Case 2. Ideal case of gravity

4 25 08 2d.jpg
Figure 4.25.08.2: Total Deformation in analysis Case 2


The remaining pictures with X, Y, Z Deformations are available atRemaining pictures of Case_2 The analysis report is available at File:4 25 08 2.pdf

Case 3. Chamber 3

4 25 08 3d.jpg
Figure 4.25.08.3: Total Deformation in analysis Case 3


The remaining pictures with X, Y, Z Deformations are available atRemaining pictures of Case_3 The analysis report is available at File:4 25 08 3.pdf

Case 4. Chamber 4

4 25 08 4d.jpg
Figure 4.25.08.4: Total Deformation in analysis Case 4


The remaining pictures with X, Y, Z Deformations are available atRemaining pictures of Case_4 The analysis report is available at File:4 25 08 4.pdf

Case 5. Chamber 5

4 25 08 5d.jpg
Figure 4.25.08.5: Total Deformation in analysis Case 5


The remaining pictures with X, Y, Z Deformations are available atRemaining pictures of Case_5 The analysis report is available at File:4 25 08 5.pdf