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QUESTION
Figure 1, shows a bracket used on a B 737 fuselage. There are 11 rivets, each of 4 mm diameter. The shear stress is 180 MPa.
1. Figure 1, shows a bracket used on a B 737 fuselage. There are 11 rivets, each of 4 mm diameter. The shear stress is 180 MPa. What is the maximum load theory states it can withstand and assuming a safety-factor of 2.5, what is it in practice?
