monk1999
Mechanical
- Feb 27, 2017
- 10
Hi,
When you try to compare the combined ring-shell sections, the required moment of inertia is I's formula which is straight forward. But when calculating the combined ring-shell section I' - what is the cross sectional area of the shell section contributing to the moment of inertia? Is it the nominal shell thickness (ts) * 1.10*sqrt(Do*ts) or ts minus the thickness required to withstand external pressure * 1.1*sqrt(Do*ts)?
Regards,
Monk
When you try to compare the combined ring-shell sections, the required moment of inertia is I's formula which is straight forward. But when calculating the combined ring-shell section I' - what is the cross sectional area of the shell section contributing to the moment of inertia? Is it the nominal shell thickness (ts) * 1.10*sqrt(Do*ts) or ts minus the thickness required to withstand external pressure * 1.1*sqrt(Do*ts)?
Regards,
Monk