Anybody help with these questions?

  • Thread starter scw1
  • Start date
In summary, the conversation discusses the maximum uniform internal pressure that a spherical pressure vessel is intended to contain, based on a design that ensures tensile stresses do not exceed 150MPa. The equation for this calculation is σ= (Pr)/t or P = σt/r, where r is the radius and t is the wall thickness. The question also clarifies that the ratio of radius to wall thickness is 100. Some participants in the conversation provide corrections to the equation, which should be σ = p*r/(2*t).
  • #1
scw1
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0
Anybody help with these questions?

Homework Statement



A spherical pressure vessel has been designed such that the tensile stresses in its walls should not exceed 150MPa. The ratio of the vessels radius to wall thickness is 100. Applying a thin-walled plane stress assumption, what is the maximum uniform internal pressure that the vessel is intended to contain?

Homework Equations



Thin walled pressure cylinder assumption P= sigma(s) x radius/2xt(s)

The Attempt at a Solution


i tried the answer 0.15MPa but not sure if its right can anyone help me??
 
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  • #2


Your equation should read σ= (Pr)/t or P = σt/r
 
  • #3


rock.freak667 said:
Your equation should read σ= (Pr)/t or P = σt/r
Hi how do you denote the radius to wall thickness, is it 100 to 1 or 10 to 0.1?
Many thanks
Stevo
 
  • #4


scw1 said:
Hi how do you denote the radius to wall thickness, is it 100 to 1 or 10 to 0.1?
Many thanks
Stevo

since r is the radius and t is the wall thickness

radius to wall ratio = 100 OR r/t = 100.
 
  • #5
Good advice by rock.freak667, except the equation should be sigma = p*r/(2*t).
 
  • #6


nvn said:
Good advice by rock.freak667, except the equation should be sigma = p*r/(2*t).

Yes it should, I was thinking about a thin-walled cylinder.
 

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