Anybody help with these questions?

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AI Thread Summary
The discussion centers on calculating the maximum uniform internal pressure for a spherical pressure vessel designed to maintain tensile stresses below 150 MPa, with a radius-to-wall thickness ratio of 100. Participants clarify the correct formula for pressure, which is P = σt/r, and confirm the ratio is expressed as r/t = 100. There is some confusion regarding the initial pressure calculation, with one user suggesting 0.15 MPa and seeking validation. The conversation emphasizes the importance of using the correct equation and understanding the ratio notation. Accurate calculations are crucial for ensuring the vessel's structural integrity under pressure.
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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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Your equation should read σ= (Pr)/t or P = σt/r
 


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
 


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


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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