Shafts · Nominal combined stress

Shaft Combined Bending and Torsion Calculator

Mechanical Engineering Calculators for nominal bending and torsional shaft stress, principal stress, maximum shear, and von Mises and Tresca equivalent stress.

Reference calculator #022

Enter section moments and circular-shaft geometry

Inputs stay in your browser. Values are normalized to canonical units before calculation.

Choose a solid or concentric hollow circular section.

Enter the resultant bending moment at the evaluated section after resolving bending components. Use zero for pure torsion.

Enter the torque magnitude at the same section. Use zero for pure bending.

Use the circular-section outside diameter at the evaluated location.

This value is ignored for a solid shaft; use d = 0 for a clean shareable state.

Display nominal component, principal, maximum-shear, and equivalent stresses in the selected unit.

Display the nominal principal-plane orientation in degrees or radians.

Calculated output

Results

shaft-combined-bending-torsion/1.0.0
Nominal von Mises equivalent stress137.832224 MPa
Nominal Tresca equivalent stress
143.460327 MPa
Nominal outer-surface bending stress σ_b
119.366207 MPa
Nominal outer-surface torsional shear stress τ_t
39.788736 MPa
Maximum principal stress σ₁ at tensile-side surface
131.413267 MPa
Minimum principal stress σ₂ at tensile-side surface
-12.04706 MPa
Maximum shear stress from the nominal surface state
71.730164 MPa
Principal-plane angle from the bending normal plane
16.845034 °
Area second moment for bending I
125663.706 mm⁴
Polar second moment for torsion J
251327.412 mm⁴
Effective inner-to-outer diameter ratio d / D
0%

Valid nominal elastic combined bending-torsion stress result

Circular shaft under combined bending and torsionA circular shaft section with bending and torque arrows beside bars comparing nominal bending, torsional, von Mises, and Tresca stresses.M = 750 N·mT = 500 N·mD = 40 mmd = 0 mmSolid circular shaftNominal outer-surface stress comparisonBending normal stress σ_b119.366207 MPaTorsional shear stress τ_t39.788736 MPavon Mises equivalent stress137.832224 MPaTresca equivalent stress143.460327 MPaσ₁ = 131.413267 MPaτ_max = 71.730164 MPaPrincipal plane = 16.845034 °
Nominal elastic stresses at the tensile-side outer surface. The comparison does not apply stress-concentration factors or determine material acceptability.
Scope and assumptions
  • The bending input is the resultant bending-moment magnitude at the evaluated section and produces the reported positive tensile-side nominal surface stress; the opposite surface has equal nominal compression from bending alone.
  • The torque input is the constant torque magnitude at the same section, and bending and torsional stresses are combined by linear-elastic superposition at the outer surface.
  • The shaft is straight, prismatic, homogeneous, isotropic, and circular with constant concentric outer and inner diameters at the evaluated section.
  • Principal, maximum-shear, von Mises, and Tresca results are calculated from the nominal plane-stress state σx = σ_b, σy = 0, and τxy = τ_t.
  • No theoretical or fatigue stress-concentration factor is applied. Keyways, splines, shoulders, grooves, holes, threads, fillets, fits, and surface condition are excluded.
  • Material strength, yield or fatigue allowables, safety factors, mean and alternating stress, combined axial or transverse shear, dynamics, deflection, critical speed, and approval are excluded.

Calculation engine: shaft-combined-bending-torsion/1.0.0

Combined-stress equations

For a solid or concentric hollow circular shaft, the centroidal area second moment I and polar second moment J are:

I = π(D⁴ − d⁴) / 64     J = π(D⁴ − d⁴) / 32 = 2I

At outer radius c = D/2, the nominal stress magnitudes are:

σ_b = Mc / I     τ_t = Tc / J

The calculator combines the tensile-side outer-surface state σx = σ_b, σy = 0, and τxy = τ_t:

σ₁,₂ = σ_b/2 ± √[(σ_b/2)² + τ_t²]
τ_max = √[(σ_b/2)² + τ_t²]
σ_vM = √(σ_b² + 3τ_t²)     σ_Tresca = √(σ_b² + 4τ_t²)
Symbol Meaning Canonical calculation unit
M Resultant bending-moment magnitude at the section N·m
T Torque magnitude at the same section N·m
D, d Concentric outer and inner diameters mm, converted to m in stress equations
σ_b, τ_t Nominal tensile-side component stresses Pa
σ₁, σ₂, τ_max Principal and maximum-shear results for that state Pa
σ_vM, σ_Tresca Nominal equivalent stresses Pa

Worked solid-shaft example

Use the default inputs: M = 750 N·m, T = 500 N·m, D = 40 mm, and d = 0.

  1. The section properties are I = 125,663.706 mm⁴ and J = 251,327.412 mm⁴.
  2. The tensile-side outer-surface stresses are σ_b = 119.366207 MPa and τ_t = 39.788736 MPa.
  3. The principal stresses are σ₁ = 131.413267 MPa and σ₂ = −12.047060 MPa.
  4. The maximum shear stress is 71.730164 MPa, and the principal plane is 16.845034° from the bending normal plane for the reported positive shear convention.
  5. The nominal equivalent stresses are σ_vM = 137.832224 MPa and σ_Tresca = 143.460327 MPa.

No material strength is entered, so the example does not state whether the shaft is acceptable.

Interpret von Mises and Tresca without inventing an allowable

Von Mises and Tresca reduce a multiaxial nominal stress state to scalar values commonly used with ductile-material yielding criteria. They are not material properties and do not become safety factors by themselves. Compare only the criterion required by the applicable design method with verified material data, temperature and condition adjustments, load factors, concentration treatment, and the required safety basis.

The Tresca equivalent stress reported here is σ₁ − σ₂, equal to twice the maximum shear for this plane-stress state. It is normally at least as large as the corresponding von Mises result, but that does not authorize choosing either criterion without a project-specific basis.

Pure bending and pure torsion limits

Set T = 0 for pure bending. The von Mises and Tresca equivalent stresses then both equal |σ_b|. Set M = 0 for pure torsion. Von Mises becomes √3 τ_t, while Tresca becomes 2τ_t. At least one load must remain positive.

If bending occurs about two perpendicular axes, first determine the resultant bending moment magnitude at the evaluated section from the complete shaft free-body diagram. This tool does not derive bearing reactions, gear forces, belt forces, moment diagrams, or the critical section.

Nominal stress is not peak local stress

The uniform circular-section equations do not represent peak stress at a keyway, shoulder, snap-ring groove, thread, spline, cross-hole, press fit, weld, or fillet. Apply the theoretical and fatigue concentration treatment required by the chosen shaft-design method. Do not insert an unverified factor merely to make the displayed value appear conservative.

Engineering scope and limitations

This calculator covers a straight, prismatic, homogeneous, isotropic, solid or concentric hollow circular shaft under a resultant bending-moment magnitude and a torque magnitude at one section. It uses linear-elastic nominal stress superposition. It excludes:

  • axial force, transverse shear stress, bearing contact, local load introduction, and noncircular sections;
  • keyways, splines, cross-holes, shoulders, grooves, threads, fillets, welds, fits, notches, and stress-concentration factors;
  • material selection, yield or ultimate strength, allowable stress, safety factors, yielding, plasticity, fracture, and final acceptance;
  • mean and alternating stress, fatigue, load spectra, reversal, shock, impact, surface finish, size effect, reliability, and residual stress;
  • deflection, slope, bearing reactions, gear or belt forces, critical speed, lateral whirl, torsional vibration, resonance, damping, and transient response;
  • tolerances, corrosion allowance, heat treatment, inspection, stock availability, manufacturing feasibility, cost, certification, and engineering approval.

Use a complete shaft free-body diagram, the governing design standard or company method, verified project data, and qualified engineering review before releasing a drawing or selecting a safety-critical shaft.

Frequently asked questions

How are bending and torsion combined for a circular shaft?

The calculator evaluates nominal bending normal stress and torsional shear stress at the tensile-side outer surface, then treats them as one plane-stress state to calculate principal, maximum-shear, von Mises, and Tresca results.

Should I compare von Mises or Tresca stress with material strength?

Use the criterion required by the governing design method and verified material basis. This calculator reports both nominal equivalent stresses but does not select an allowable, safety factor, or acceptance criterion.

Does the calculator include a keyway or shaft shoulder?

No. It uses a uniform circular section and applies no theoretical or fatigue stress-concentration factor. Evaluate keyways, shoulders, grooves, holes, splines, threads, and fillets separately.

Can either bending moment or torque be zero?

Yes. Zero torque produces the pure-bending limit, and zero bending moment produces the pure-torsion limit. At least one load magnitude must be positive.

Does the maximum bending stress occur at every point around the shaft?

No. For a given bending-moment direction, its magnitude is greatest at the two outer fibers on the bending plane. The calculator reports the tensile-side state; the opposite side has the corresponding compressive bending stress and a different principal-stress sign pattern.

References and review status

Reviewed . References support nominal elastic circular-shaft section properties, combined plane stress, principal stress, and equivalent-stress equations. They do not establish material allowables, fatigue strength, concentration factors, or shaft approval.