Tensile Strength Calculator

Enter a force and a cross-section (diameter, width × thickness, rebar or bolt size) to get tensile stress in MPa and psi, compare it with the yield and ultimate strength of steel, aluminum, bolts and more, and see the load at yield and at break.

Tensile stress σ = F ÷ A.

Use the Tensile Strength Calculator

Input Parameters

Area in mm²

Enter a force and a cross-section, then click Calculate.

Tensile strength of common materials — yield vs UTS

Yield strength, ultimate tensile strength (UTS), Young's modulus and elongation at break. Steels and fasteners show specification minimums (ASTM A36, A992, A615, A240, SAE J429, ISO 898-1); the others are typical handbook values. Use certified mill or supplier values for design.

Yield strength, ultimate tensile strength, Young's modulus and elongation of common materials
MaterialBasisYield MPa (ksi)UTS MPa (ksi)E (GPa)Elongation %
A36 structural steelASTM A36, min.250 (36)400 (58)20020–23
A992 structural steel (W-shapes)ASTM A992, min.345 (50)450 (65)20018–21
Grade 60 rebarASTM A615 Gr 60, min.414 (60)621 (90)2007–9
1018 carbon steel, cold drawnAISI 1018, typical370 (54)440 (64)20515
4140 alloy steel, annealedAISI 4140, typical415 (60)655 (95)20526
304 stainless steel, annealedASTM A240, min.205 (30)515 (75)19340
Bolt, property class 8.8 (≤ M16)ISO 898-1, min.640 (93)800 (116)20012
Bolt, property class 10.9ISO 898-1, min.940 (136)1040 (151)2009
Bolt, SAE Grade 5 (¼–1 in)SAE J429, min.634 (92)827 (120)20014
Bolt, SAE Grade 8SAE J429, min.896 (130)1034 (150)20012
Aluminum 6061-T6Typical276 (40)310 (45)68.912
Aluminum 7075-T6Typical503 (73)572 (83)71.711
Titanium Ti-6Al-4V (Grade 5), annealedTypical880 (128)950 (138)113.814
Copper C11000, annealedTypical69 (10.0)220 (32)11545
Gray cast iron, class 30ASTM A48, min.—207 (30)100< 1
Nylon 6/6, dryTypical—80 (11.6)350+

Rebar and bolt areas

Nominal rebar areas and bolt tensile stress areas
SizeArea (mm²)Area (in²)Group
#3 rebar (3/8 in)71.00.11ASTM rebar
#4 rebar (1/2 in)1290.2ASTM rebar
#5 rebar (5/8 in)2000.31ASTM rebar
#6 rebar (3/4 in)2840.44ASTM rebar
#7 rebar (7/8 in)3870.6ASTM rebar
#8 rebar (1 in)5100.79ASTM rebar
#9 rebar6451ASTM rebar
#10 rebar8191.27ASTM rebar
#11 rebar1,0061.56ASTM rebar
M6 bolt20.10.0312Metric bolts (stress area)
M8 bolt36.60.0567Metric bolts (stress area)
M10 bolt58.00.0899Metric bolts (stress area)
M12 bolt84.30.1307Metric bolts (stress area)
M16 bolt1570.2434Metric bolts (stress area)
M20 bolt2450.3798Metric bolts (stress area)
M24 bolt3530.5472Metric bolts (stress area)
1/4-20 bolt20.50.0318UNC bolts (stress area)
5/16-18 bolt33.80.0524UNC bolts (stress area)
3/8-16 bolt50.00.0775UNC bolts (stress area)
1/2-13 bolt91.50.1419UNC bolts (stress area)
5/8-11 bolt1460.226UNC bolts (stress area)
3/4-10 bolt2150.334UNC bolts (stress area)
1-8 bolt3910.606UNC bolts (stress area)

Rebar: ASTM A615 nominal areas. Bolts: tensile stress area As (ISO 898-1 coarse thread; ASME B1.1 UNC), which is smaller than the shank area. 1 ksi = 6.895 MPa; 1 in² = 645.16 mm².

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Quick answer

Tensile stress σ = F ÷ A. A 10 mm round bar has A = π × 5² = 78.54 mm², so a 20 kN pull gives 20,000 N ÷ 78.54 mm² = 254.6 MPa (36.9 ksi), just above the 250 MPa yield of A36 steel. Tensile strength (UTS) is the highest stress before it breaks, so breaking load = UTS × A: with A36's 400 MPa minimum UTS that bar breaks at about 31.4 kN. Design to the yield strength with a safety factor.

Examples

PartAreaYield loadBreaking load
10 mm A36 steel rod78.54 mm²19.6 kN (250 MPa)31.4 kN (400 MPa)
#5 Grade 60 rebar0.31 in²18.6 kip (60 ksi)27.9 kip (90 ksi)
M12 class 8.8 bolt84.3 mm²54.0 kN (640 MPa)67.4 kN (800 MPa)
1/2-13 SAE Grade 5 bolt0.1419 in²13.1 kip (92 ksi)17.0 kip (120 ksi)
6061-T6 aluminum, 20 × 5 mm bar100 mm²27.6 kN (276 MPa)31.0 kN (310 MPa)

Enter the force and the section, pick a material, and see stress, safety factor and the yield and breaking loads.

Summary

Tensile stress is the pulling force divided by the cross-sectional area, σ = F/A. Whether a part holds depends on how that stress compares with the material: the yield strength, where permanent stretching starts, and the ultimate tensile strength (UTS), the peak stress before fracture. This calculator takes the force and the section (direct area, round bar, rectangle, ASTM rebar size or a bolt tensile stress area), gives the stress in MPa, Pa, psi and ksi, and with a material picked shows the utilization, safety factor to yield and to UTS, and the load at yield and at break. Add the gauge length and elongation from a test to get strain, elongation % and Young's modulus. Material values are typical or specification minimums from ASTM, SAE and ISO standards and handbooks; use the certified values for design.

How it works

  1. Pick SI (N, mm) or Imperial (lbf, in) units.
  2. Enter the tensile force.
  3. Enter the area directly, or a round bar diameter, a rectangle width × thickness, or choose a rebar or bolt size to fill in its area.
  4. Optionally pick a material to compare the stress with its yield strength and ultimate tensile strength.
  5. Optionally enter the gauge length and measured elongation to get strain, elongation % and Young's modulus.
  6. Click Calculate to see stress, safety factors, the load at yield and at break, and the strain results.

Use cases

  • Checking whether a rod, bar, wire or bolt will yield or break under a given pull.
  • Finding the breaking load of a steel rod or rebar from its diameter and grade.
  • Comparing bolt grades (class 8.8, 10.9, SAE Grade 5, Grade 8) for the same load.
  • Turning tensile test load and extension data into stress, strain and modulus.
  • Mechanics of materials homework on σ = F/A, ε = ΔL/L₀ and E = σ/ε.
  • Estimating the safety factor of a hanger, tie rod or eye bolt.

Frequently Asked Questions

Last updated: 2026-10-10 · Reviewed by Nham Vu