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MECHANICS

Firstly, the structural behaviour is analysed when

the wind load is applied from the top. From the

results of the table, it can be seen that with this

wind load direction, the simplification into an arch

and a rectangle is not totally effective, because

the values of bending moments, stresses and

deflection differ a lot from the real model. In this

case, the FEA seems to have more reasonable

results and therefore, be more reliable for real

situation behaviour.

The assumption of 5mm thickness from hand

calculations seems to be sufficient against breaking

load, but with big consequences in deflection.

Therefore, further FEA was needed, where the

thickness of the material was increased steadily.

In the end, a thickness of 7,5 mm was found to be

the most suitable, with a final deformation of 1,8

mm.

FIGURE 78: DIANA STRESSES TOP LOAD

FIGURE 79: DIANA DEFLECTIONS TOP LOAD

Top Wind Load

Results Improved DIANA Required

σ max 9x 10 -3 N/m 2 <310 N/m 2

δ max 1.8 mm <2 mm

FIGURE 80: CASE 2A - DIANA TOP LOAD IMPROVED

TABLE 13: CASE 2A RESULTS IMPROVED TOP WIND LOAD - B= 7.5MM

52

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