Your Equation

Library / Mechanical / MEC-48

Mechanical

Thin-walled cylinder axial stress

Axial stress in a thin-walled cylinder with closed ends carrying the pressure thrust.

Ref
MEC-48
Rev
v1
Field
Mechanical
Result
σz [MPa]

With closed ends the pressure acts on the end area πa² and the thin wall, of area about 2πat, carries the thrust: σz = pπa²/(2πat) = pa/(2t). p is the internal gauge pressure, a the internal radius (di = 2a) and t the wall thickness. For open ends with no axial load, σz = 0. It is half the thin-wall hoop stress, which is why the hoop stress sets the wall thickness.

Axial stress in a thin-walled cylinder with closed ends carrying the pressure thrust. It is half the hoop stress. For open ends with no axial load it is zero.

Calculator

Solve for
MPa
MPa
0.120
mm
1002,000
mm
150
  • Pressure thrust on the end, pπa²1,571 kN
  • Hoop stress pa/t, twice the axial stress100 MPa

What drives the result

Each variable is moved across its typical range while the others stay at the values above. The longest bar is the key driver.

Axial stress (MPa) current value 50 MPa
pInternal gauge pressureKey driver
2.5500
tWall thickness
10500
aInternal radius
10200
  • The axial stress of 50 MPa is exactly half the 100 MPa hoop stress, so the hoop stress sets the design thickness and the axial stress is a secondary check.
  • The end thrust is large: about 1571 kN at the defaults, carried by a wall area of only about 31 400 mm². The end caps, flanges and bolts must carry the same force.
Chart data as tables

Ranked variables

VariableTypical rangeLowest resultHighest resultSwing (MPa)Local stepChange in result
p Internal gauge pressure0.1 to 20 MPa2.5500497.5+10%+10 %
t Wall thickness1 to 50 mm10500490+10%−9.09 %
a Internal radius100 to 2,000 mm10200190+10%+10 %

Sweep of Wall thickness

Wall thickness (mm)Axial stress (MPa)
1500
7.12570.18
13.2537.74
19.3825.81
25.519.61
31.6315.81
37.7513.25
43.8811.4
5010

Sweep one variable

Axial stress (MPa)Hover, touch, or use the arrow keys on the chart
0100200300400500 1020304050 Wall thickness (mm) now 50

Variables and how each one contributes

σz

Axial stress

Result · MPa

What the equation gives you. Everything else feeds it.

p

Internal gauge pressure

MPa · typical 0.1 to 20

The internal gauge pressure, in MPa. Directly proportional: a 10 % rise in p raises the axial stress by 10 %.

a

Internal radius

mm · typical 100 to 2,000

The internal radius, in mm. Directly proportional: a 10 % rise in a (to 550 mm) raises the axial stress by 10 %, to 55 MPa, since the end area grows as a² while the wall grows as a.

t

Wall thickness

mm · typical 1 to 50

The wall thickness, in mm. Inversely proportional: a 10 % rise in t (to 11 mm) lowers the axial stress by 9 %, to 45.5 MPa.

Worked example with the values above

  1. End thrust: F = pπa² = 2 × π × 500² = 1,571,000 N.
  2. Wall area: 2πat = 2π × 500 × 10 = 31,420 mm².
  3. σz = 1,571,000 / 31,420 = 50 MPa, which equals pa/(2t).

Assumptions and limits

  • A thin wall (t/a well under 0.1) with closed ends that carry the pressure thrust and no other axial load.
  • A section away from the ends and nozzles, with uniform stress through the wall thickness.

Common mistakes

  • Applying it to an open-ended pipe, which has no axial stress unless an axial load acts on it.
  • Forgetting the factor 2 and quoting the hoop stress as the axial stress.

Statistics and uncertainty

σz = pa/(2t) has the same sensitivity as the hoop stress: errors in p and a pass through proportionally and t enters inversely, so ±10 % wall thickness gives about ±10 % in σz. In practice the pressure often has peaks above the nominal value, which matters more than the small errors in the dimensions.

Where it is used

  • Sizing end caps, flanges and bolts for the end thrust of a pressure vessel.
  • Axial stress in tanks and gas bottles, as an input to a Tresca or von Mises check.

Maths you need

  • Force balance: end thrust equals wall force
  • Area of a thin ring: 2πat

Related formulas

Practise this formula