Pressure vessel classification: a cylindrical shell is classed as a “thick” shell when the ratio of its internal diameter to wall thickness (D/t) is approximately below which value?

Difficulty: Easy

Correct Answer: D/t less than about 10

Explanation:


Introduction / Context:
Pressure vessel analysis distinguishes between thin and thick cylinders because stress distributions differ significantly. Thin-shell formulas assume negligible radial stress variation, while thick-shell theory (e.g., Lame’s equations) accounts for radial gradients and is needed when walls are relatively thick.



Given Data / Assumptions:

  • Internal pressure service with cylindrical geometry.
  • D denotes internal diameter; t denotes wall thickness.
  • Standard engineering thresholds used for preliminary classification.


Concept / Approach:
A common rule places thin-shell validity when t ≤ D/20 (i.e., D/t ≥ 20). As the wall becomes thicker (smaller D/t), thin-shell assumptions break down and thick-shell analysis is required. Some practices use a stricter threshold near D/t ≈ 10 for conservative classification of “thick” shells.



Step-by-Step Solution:

Relate thickness to diameter via D/t.If D/t is small (wall relatively thick), radial stress variation is appreciable.Adopt thick-shell treatment for D/t roughly below 10; use thin-shell formulas for D/t around 20 or higher.


Verification / Alternative check:
Design texts show thin-shell hoop stress σ_h = P D /(2 t) applies well when t ≤ D/20; for thicker walls, Lame’s solution is recommended.



Why Other Options Are Wrong:

  • “D/t greater than 10 or 20” indicate thin walls; thick-shell classification applies to smaller D/t, not larger.
  • “D/t less than about 20” is broader and includes some thin-shell range; the more accepted “thick” cutoff is nearer 10.


Common Pitfalls:
Using thin-shell equations outside their range; forgetting joint efficiency and corrosion allowance implications; ignoring external pressure buckling checks.



Final Answer:
D/t less than about 10

Discussion & Comments

No comments yet. Be the first to comment!
Join Discussion