Strain gauges · Measurement

Separating axial force and bending: four gauges around a bar

From four longitudinal gauges at 0°, 90°, 180° and 270° of a mast or bar section, compute the axial strain, bending strains in two planes, the bending-plane orientation and the resulting stresses.

DMSKeil 2017
01

Inputs

Circular or doubly symmetric section, gauges exactly 90° apart at equal radius, no torsion effect on longitudinal gauges and no temperature difference between gauge locations.

02

Results

Enter values and run the calculation.

Method

What is calculated?

For a slender bar under axial force and bending the axial direction is principal; each longitudinal gauge measures the sum of the normal strain and the bending component at its circumferential position. Two opposite gauges share the normal part but have opposite bending parts, so mean and half difference separate the components. Keil's mast example (Tab. 10.1) with −246/−340/−324/−241 µm/m yields −288 µm/m compression plus bending components aft and to port.

Equations

ε_N = (ε₁+ε₂+ε₃+ε₄)/4

ε_b,x = (ε₁−ε₃)/2, ε_b,y = (ε₂−ε₄)/2

ε_b = √(ε_b,x² + ε_b,y²), φ = atan2(ε_b,y, ε_b,x)

σ = E·ε (einachsig, Keil Tab. 10.1)

Procedure

Step by step

  1. Install four longitudinal gauges 90° apart and label them counter-clockwise.
  2. Record and enter the strains of one load case simultaneously.
  3. Compare stresses with permissible values; use the bending-plane direction to interpret the load.

Typical mistake

Not labelling the gauges in circumferential order, which corrupts the bending-plane direction.

Practice

Application and limits

Stress measurement on masts, columns, piles, tie rods and piston rods where axial force and bending superimpose.

Circular or doubly symmetric section, gauges exactly 90° apart at equal radius, no torsion effect on longitudinal gauges and no temperature difference between gauge locations.

Source

Technical basis

Keil, Dehnungsmessstreifen, 2nd ed. 2017, sec. 10.2.1 yacht-mast example, Tab. 10.1, figs. 10.3–10.5; sec. 4.5, eqs. (4.14), (4.15).

The source supports the equation structure and worked examples; this calculator does not replace calibration of the measuring chain.

FAQ

Frequently asked questions

Why four gauges instead of two?

Two opposite gauges separate bending in one plane only; the bending plane is usually unknown.

Can I separate the components electrically?

Yes: gauges 1 and 3 in opposite arms (circuit VI) give 2ε_N, in adjacent arms (IV) 2ε_b.

What about temperature?

A common compensation gauge on unloaded bar material, as in Keil's example, cancels the temperature response for all four points.