Given data follows below:
Long aluminum tube =200-mm
Diameter closed at its ends =100 mm
Wall thickness of = 2 mm
Internal pressure of = 4 MN/m
U = 3 and
E = 70 X 10 N/m .
Now calculating longitudinal stresses
pd/4t = (4x106 N/m2)(100x10-3m) / 4x2x10-3m
= 0.5 x 108 N/m^2
= 50 MPa
Now calculating tangential stresses at an 2192
pd/2t = (4x106 N/m2)(100x10-3m) / 2x2x10-3m
= 108 N/m^2
= 100 MPa
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