Weld Strength Calculations

This page provides practical methods for calculating weld strength including fillet and butt welds under direct load, bending and torsion based on BS 5950 design principles.

Weld strength calculations are based on weld size, material strength and loading conditions, using stress analysis for shear, bending and torsion.

This page provides practical methods for calculating weld strength including fillet and butt welds under direct load, bending and torsion based on BS 5950 design principles.

Weld strength calculations are based on weld size, material strength and loading conditions, using stress analysis for shear, bending and torsion.

Contents

1. Introduction
2. Relevant Standards
3. Variables Associated With Welds
4. Guidance Principles
5. Table Basic Weld Calcs.
6. Assessment of Fillet Welds
7. Examples of Fillet Welds Calcs
8. Properties of Fillet Welds as lines
9. Example of torsion weld calc. using vectors
10. Capacities of Fillet Welds

Introduction

What Determines Weld Strength?

• Weld size (throat thickness and leg length)
• Material strength and electrode classification
• Type of loading (shear, bending, torsion)
• Weld geometry and location
• Safety factors and design standards

The following notes are general guidance notes showing methods of calculation of the strength and size of welds.  Welded joints are often crucially important affecting the safety of the design systems.  It is important that the notes and data below are only used for preliminary design evaluations.  Final detail design should be completed in a formal way using appropriate codes and standards and quality reference documents

Interactive Weld Calculators

RoyMech now includes interactive weld calculators for fillet weld strength, weld throat area, rectangular weld groups and circular weld groups. These calculators show the formulae used, substituted values, worked calculations and allow the results to be printed or saved as a PDF.

Calculator	Use
Fillet Weld Strength & Size Calculator	Calculate fillet weld throat area, weld shear stress, utilisation and required weld size for direct shear loading.
Weld Throat Area Calculator	Calculate effective throat thickness, area of one weld and total effective throat area.
Rectangular Weld Group Properties Calculator	Calculate weld length, throat area, centroid, Ixx, Iyy and polar moment for closed rectangular weld groups.
Rectangular Weld Group Stress Calculator	Calculate rectangular weld group direct shear stress, torsional shear stress, maximum resultant stress and utilisation.
Circular Weld Group Properties Calculator	Calculate circular weld length, effective throat area, centroid and polar moment of inertia.
Circular Weld Group Stress Calculator	Calculate circular weld group direct shear stress, torsional shear stress, maximum resultant stress and utilisation.

View all RoyMech Weld Calculators

Relevant Standards

BS 5950-1:2000 has been replaced by BS EN 1993..Structural use of steelwork in building. Code of practice for design. Rolled and welded sections
BS EN 10025-1:2004 - Hot rolled products of structural steels. General technical delivery conditions

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Variables Affecting Weld Strength

Strength of deposited weld material Type of joint and weld..important Size of weld ..important Location of weld in relation to parts joined..important Types of stress to which the weld is subjected Conditions under which weld is carried out Type of equipment used for welding Skill of welder

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Weld Design Principles

A generous factor of safety should be used (3-5) and if fluctuating loads are present then additional design margins should be included to allow for fatigue

Use the minimum amount of filler material consistent with the job requirement

Try to design joint such that load path is not not through the weld

The table below provides provides approximate stresses in, hopefully, a convenient way.

For the direct loading case the butt weld stresses are tensile/ compressive σ _t for the fillet welds the stresses are assumed to be shear τ _s applied to the weld throat.

For butt welded joints subject to bending the butt weld stresses result from a tensile/compressive stress σ _b and a direct shear stress τ _s .
In these cases the design basis stress should be σ _r = Sqrt (σ _b² + 4τ _s²)

For Fillet welded joints subject to bending the stresses in the fillet welds are all shear stresses.   From bending τ _b and from shear τ _s
In these cases the design basis stress is generally τ _r =Sqrt (τ _b² + τ _s²)

The stresses from joints subject to torsion loading include shear stress from the applied load and shear stresses from the torque loading.  The resulting stresses should be added vectorially taking care to choose the location of the highest stresses.

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Table of bracket weld subject to direct and bending stresses

Method of Loading	Weldment	Stress in Weld σb τs Weld size (h)	Weldment	Stress in Weld σb τs Weld size (h)	Weldment	Stress in Weld τb τs Weld size (h)
		Direct tensile stress in weld: σt = P / (b h) Required weld size: h = P / (b σt)		Combined tensile stress in weld: σt = 0.5P / (b h) Required weld throat thickness: h = 0.5P / (b σt)		Shear stress in weld: τs = 0.71P / (b h) Required weld size: h = 0.71P / (b τs)
		Bending stress in weld: σb = (6 P A) / (b h²) Direct shear stress: τs = P / (b h) Required weld size: h = √((6 P A) / (b σb))		Section modulus parameter: x = d³ − (d − 2h)³ Bending stress: σb = (6 P A d) / (b x) Shear stress: τs = P / (2 b h)		Polar section parameter: x = (d + 2h)³ − d³ Torsional shear stress: τb = (8.5 P A d(d + 2h)) / (b x) Direct shear stress: τs = 0.71P / (b h)
		Bending stress: σb = (6 P A) / (h d²) Shear stress: τs = P / (d h) Required weld size: h = (6 P) / (σb d²)		Bending stress: σb = (3 P A) / (h d²) Shear stress: τs = P / (2 d h) Required weld size: h = (3 P A) / (σb d²)		Torsional shear stress: τb = (4.24 P A) / (h d²) Direct shear stress: τs = 0.71P / (h d) Required weld size: h = (2.12 P A) / (τb d²)
				Geometric parameter: x = (b − 2h)(d − 2h)³ y = (b − 2h)(d − 2h) Bending stress: σb = (6 P A d) / (b d³ − x) Shear stress: τs = P / (b d − y)		Geometric parameter: x = (b + 2h)(d + 2h)³ y = (b + 2h)(d + 2h) Torsional shear stress: τb = (8.49 P A d) / (x − b d³) Direct shear stress: τs = (1.41 P) / (y − b d)

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Assessment of Fillet Weld Groups

ref notes and table Properties of Fillet Welds as lines

Important note: The methods described below is based on the simple method of calculation of weld stress as identified in BS 5950- clause 6.7.8.2 . The other method identified in BS 5950 - 1 clause 6.7.8.3 as the direction method uses the method of resolving the forces transmitted by unit thickness welds per unit length into traverse forces (F_T ) and longitudinal forces (F_L ).  I have, to some extent, illustrated this method in my examples below

The method of assessing fillet welds groups treating welds as lines is reasonably safe and conservative and is very convenient to use.

a) Weld subject to bending....See table below for typical unit areas and unit Moments of Inertia

A fillet weld subject to bending is easily assessed as follows.

1) The area of the fillet weld A _u..(unit thickness) is calculated assuming the weld is one unit thick..
2) The (unit) Moment of Inertia I _u is calculated assuming the weld is one unit thick..
3) The maximum shear stress due to bending is determined...τ _b = M.y/I _u
4) The maximum shear stress due to direct shear is determined.. τ _s = P /A
5) The resultant stress τ _r = Sqrt (τ _b² + τ _s² )
6) By comparing the design strength p _w with the resultant stress τ _r the value of the weld throat thickness is calculated and then the weld size.
i.e. if the τ _r /p _w = 5 then the throat thickess t = 5 units and the weld leg size h = 1,414t

a) Weld subject to torsion...See table below for typical unit areas and unit Polar moments of Inertia

A fillet weld subject to torsion is easily assessed as follows.

1) The area of the fillet weld A _u (unit thickness) is calculated assuming the weld is one unit thick
2) The (unit) Polar Moment of Inertia J _u is calculated assuming the weld is one unit thick..   The polar moment of inertia J = I _xx + I _yy
3) The maximum shear stress due to torsion is determined...τ _t = T.r/J _u
4) The maximum shear stress due to direct shear is determined.. τ _s = P /A _u
5) The resultant stress τ _r is the vector sum of τ _t and τ _s.  r is chosen to give the highest value of τ _r
6) By comparing the design strength p _w with the resultant stress τ _r the value of the weld throat thickness is calculated and then the weld size.
i.e. if the τ _r /p _w = 5 then the throat thickness t = 5 units and the weld leg size h = 1,414.t

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Worked Examples of Fillet Weld Calculations

Example of Weld in Torsion.. P = Applied load = 10 000N P w = Design Strength = 220 N/mm 2 (Electrode E35 steel S275)   Design Strength b = 120mm. d = 150 mm x = b2 / 2(b+d) = 27mm.. (From table below) y = d2 / 2(b+d) = 42mm..(From table below) Simple Method as BS 5950 clause 6.8.7.2 ..The vector sum of the stresses due to forces and moments should not exceed the design strength Pw A u = Unit Throat Area = (From table below) b + d = (120 + 150) = 270mm2 To obtain radius of Force from weld centre of gravity A = 250-27 =223mm Moment M = P.r = 10000.223 = 2,23.106 N.mm J u = [(b+d)4 - 6b2d2] /12 (b+d) = 1,04.106..(From Table) It is necessary to locate the point subject to the highest shear stress..For a weld subject to only torsion this would be simply at the point furthest from the COG.   However because the weld is subject to torsion and direct shear the problem is more complicated.  A normal method of determining the stresses in these cases is to use vector addition. It is generally prudent to calculate the total shear stress at both positions, using the method below, and select the highest..  For this example the method used is to resolve the stresses in the x and y directions First considering point Z Horizontal distance from centroid r zh = 120-27= 93mm Vertical distance from centroid r zv = 42mm The vertical stress τ v = τ sv + τ tv τ sv = P /A u = 10000/270 = 37 N/mm2 τ tv = M.r zh /J u = 2,23.106.93/1,04.106 = 199 N/mm2 τ v = 236,45 N/mm2 The horizontal stress τ h = τ sh + τ th τ sh = 0 τ th = M.r zv /J u = 2,23.106.42/1,04.106 = 90 N/mm2 τ h = 90 N/mm2 The resultant stress on the weld at z τ r = Sqrt (τ h2 + τ v2) = 253 N/mm2 Now considering point w Horizontal distance from centroid r wh = 27mm Vertical distance from centroid r wv = 150-42= 108mm The vertical stress τ v = τ sv - τ tv τ sv = P /A u = 10000/270 = 37 N/mm2 τ tv = M.r wh /J u = 2,23.106.27/1,04.106 = 57,9 N/mm2 τ v = 20,86 N/mm2 The horizontal stress τ h = τ sh + τ th τ sh = 0 τ th = T.r wv /J u = 2,23.106.108/1,04.106 = 231,6 N/mm2 τ h = 231,6 N/mm2 The resultant stress on the weld at w τ r = Sqrt (τ h2 + τ v2) = 232,5 N/mm2 The maximum stress is similar but greatest at z .... The design strength p w for the weld material is 220 N/mm 2 The weld throat thickness should be 253 /220 = 1,15mm . The weld size is therefore 1,414. 1,15 = 1,62mm use 3mm fillet weld Direction Method as BS 5950 clause 6.8.7.3 L = Length of weld 1 unit thick = (From table below) b + d = (120 + 150) = 270mm To obtain radius of Force from weld Centre of Gravity (Cog) . A = 250-27 =223mm Moment M = P.r = 10000.223 = 2,23.106 N.mm Ju = Polar Moment of inertia for weld 1unit(mm) thick. = [(b+d)4 - 6b2d2] /12 (b+d) = 1,04.106 mm4 /mm..(From Table) It is necessary to locate the point subject to the highest shear stress..For a weld subject to only torsion this would be simply at the point furthest from the COG.   However because the weld is subject to torsion and direct shear the problem is more complicated.  A normal method of determining the stresses in these cases is to use vector addition. It is generally prudent to calculate the total shear stress at both positions, using the method below, and select the highest..  For this example the method used is to resolve the stresses in the x and y directions First considering point Z Horizontal distance from centroid r zh = 120-27= 93mm Vertical distance from centroid r zv = 42mm The vertical force /mm run F v = F sv + F tv F sv = P /L = 10000/270 = 37 N/mm run F tv = M.r zh /J u = 2,23.106.93/1,04.106 = 199 N/mm run F v = 236,45 N/mm run The horizontal force /mm run for unit(mm) weld width F h = F sh + F th F sh = 0 F th = M.r zv /J u = 2,23.106.42/1,04.106 = 90 N/mm run F h = 90 N/mm run The resultant force on the weld/mm run at z F r = Sqrt (F h2 + F v2) = 253 N/mm run Now considering point w Horizontal distance from centroid r wh = 27mm Vertical distance from centroid r wv = 150-42= 108mm The vertical forces per mm run F v = F sv - F tv F sv = P /L = 10000/270 = 37 N/mm run F tv = M.r wh /J u = 2,23.106.27/1,04.106 = 57,9 N/mm run F v = 20,86 N/mm run The horizontal force /mm run = F h = F sh + F th F sh = 0 F th = M.r wv /J u = 2,23.106.108/1,04.106 = 231,6 N/mm run F h = 231,6 N/mm run The specific force on the weld at w F r = Sqrt (F h2 + F v2) = 232,5 N/mm run The maximum specific is greatest at z = 253 N/mm run.... Referring to weld capacities for longitudinal stresses PL for fillet welds Capacities of Fillet Welds the weld capacity for a 3mm weld with and E35 Electrode S275 Steel is 462N /mm run. This weld would be more than sufficient.

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Example of Weld in Bending.. P= 30000 Newtons d= 100mm b= 75mm y = 50mm Design Stress p w = 220 N/mm 2 (Electrode E35 steel S275)   Design Strength Moment = M = 30000*60=18.10 5 Nmm Simple Method as BS 5950 clause 6.8.7.2 Unit Weld Area = A u = 2(d+b) =2(100+75) =350mm 2 Unit Moment of Inertia = I u = d 2(3b+d) / 6 = 100 2 (3.75 +100) / 6 =5,42.105 mm4 τ r = Sqrt(τ s2 + τ b2) τ s = P / A u = 30000/350 = 85,71 N/mm 2 τ b = M.y / I u = 18.105 . 50 / 5,42.105 = 166,05 N/mm 2 τ r = Sqrt(85,71 2 + 166.052) =186,86 N/mm2 τ r / p w = 186,86 / 220 = 0,85 = Throat Thickness..... ( Throat thickness for τ = 220 N/mm2 ) Leg Length = Throat thickness *1,414 = 1,2mm use 3mm weld thickness Note : If a leg length h= 1,2mm is used in the equations in relevant part of the "Table of bracket weld subject to direct and bending stresses" above a value of τ b = 198 N/mm and a value of τ s = 100 N/mm2 results with a resultant stress of Sqrt (τ b2 + τ s2) = 222N/mm2..Which is in general agreement with the above result Direction Method as BS 5950 clause 6.8.7.3 Length of Weld of unit thickness = L = 2(d+b) =2(100+75) =350mm Moment of Inertia / mm throat thickness = I u / mm   = d 2(3b+d) / 6 = 100 2 (3.75 +100) / 6 =5,42.105 mm 4 / mm F r = Resultant force per unit length of weld. F s = Shear force per unit length of weld. F b = Bending force per unit length of weld. F r = Sqrt(F s2 + F b2) F s = P / L = 30000/350 = 85,71 N per mm length of weld F b = M.y / I u    = 18.105 . 50 / 5,42.105 = 166,05 N per mm length of weld F r = Sqrt(85,71 2 + 166.052) =186,86 N per mm length of weld. For this case for the welds under greatest loading the type of loading is traverse loading. The bending stress is in line with horizontal element and the shear stress is in line with vertical member. The angle of the resulting specific load to the horizontal element = arctan(85,71/166,5)= 27,5o. This is an angle with the weld throat θ = 45o + 27,5o = 72,5o Referring to weld capacities table below.Weld Capacities K is calculated at 1,36 for this resultant direction of forces. PT = a.K.pwfor a E35 Weld electrode used with S275 steel pw = 220 N/mm2 and therefore PT = a*300N/mm2.. A 3mm weld (a = 2,1mm) therefore will therefore have a design capacity of 630 N/mm run and will easily be able to support the load of 186,86 N per mm run

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Properties of Weld Groups with Welds Treated as Lines

For many engineering weld strength calculations, weld groups may be treated as line elements with properties based on unit weld throat thickness.

Second Moment of Area About the X-X Axis

I_xx = 2 [(b d³ / 12) + b d (h + 0.5d)²]

Where weld thickness d is small compared with dimensions b and h:

I_xx ≈ 2 b h²

Second Moment of Area About the Y-Y Axis

I_yy = 2 (d b³ / 12)

Polar Moment of Inertia

J = I_xx + I_yy

This is illustrated in the tabled values below

	d	b	h	Ixx	Iyy	J= Ixx +Iyy
Accurate	3	60	50	955080	108000	1063080
Simple	3	60	50	900000	108000	1008000
Error				6%	0	5%

Note: The error identified with this method is lower as h increases relative to d.   This error is such that the resulting designs are conservative.

Example illustrating use of stress vectors

Calculation based on real weld sizes 1) The area of the welds (based on throat weld thickness at 0,707.5 = 3,5mm) Area = (57.3,5 + 2.55.3,5) = 584,5mm2 2) The moment of area about x-x = M of Area = (57.3,5.3,5/2 + 2.55.3,5.(27.5 + 3,5)) = 12 284mm3 3) The centroid v = Moment of Area/Area M of Area / Area = 21 mm 4) The radii rA, rB, rC & rD are calculated .. rA = rB = Sqrt ((58,5-21)^2 + 28,5^2 ) = 47,1 rC = rD = Sqrt ((21)^2 + 28,5^2 ) = 35,40... 5) The angles θA, θB, θC & θD are calculated .. θA = θB = tan-1 ((58,5-21)/ 28,5 ) = 52,7o θC = θD = tan-1 ((21)/28,5 ) = 36,4o... 6) The direct shear stress on the area = Force /Area τ S = 5000/584 = 8,56 N/mm2 7) The Moment on the weld group = Force.Distance to centroid M = 5000.(100+21) = 6,05.105Nmm 8) The polar moment of inertia of the weld group = J = Ixx + Iyy Iyy = 2.[55.3,53 /12 + 3,5.55.(50/2 + 3,5/2)2]    + 573.3,5/12 = 3,3.105mm4 Ixx = 2.[553.3,5/12 + 3,5.55.(55/2 + 3,5 - 21)2]    + 3,5357 / 12 + 3,5.57.(21-3,5/2)2 = 2,097 .105mm4    J = Ixx +Iyy= 5,4.105mm4 9) The stress due to torsion τ TA = τ TB = M.rA/J.. and ..τ TC = τ TD = M.rC/J τTA = 6.055Nmm.47,1mm / 5,4.105mm4=52,8 N/mm2 τTC = τ TD = 6.055Nmm.35,4mm / 5,4.105mm4= 39,70N/mm2 10) The resultant stresses τ RA, = τ RB and τ RA, =  τ RB are obtained by adding the stress vectors graphically as shown below τRA = τRB=46,29 N/mm2 τRC = τRD = = 45,31N/mm2

Calculations based on unit values This calculation uses equations from table below for Area, centroid, and Ju 1) Area of weld = 0,707.5.(2b+d) Area = 0,707.5.(2.55 + 50) = 565.6mm2 2) There is no need to calculate the Moment of Area with this method 3) The centroid v = b2 /(2b+d) v = 552/(2.55+50)= 18,9mm 4) The radii rA, rB, rC & rD are calculated .. rA = rB = Sqrt ((55-18,9)^2 + 25^2 ) = 43,9 rC = rD = Sqrt (18,9^2 + 25^2 ) = 31,34 5) The angles θA, θB, θC & θD are calculated .. θA = θB = tan-1 ((55-18,9)/ 25 ) = 55,29o θC = θD = tan-1 ((18,9)/25 ) = 37o... 6) The direct shear stress on the area = Force /Area τS = 5000/565,5 = 8,84 N/mm2 7) The Moment on the weld group = Force .distance to centroid M = 5000.(100+18,9) = 5.94.105Nmm 8) The Unit Polar moment of inertia of the weld group = Ju = 0.707.5.(8.b3 +6bd2+d3)/12 + b4/(2b+d) Ju = 0,707.5.(8.553+6.55.502 + 503)/12 - 553/(2.55+50) = 4,69.105 9) The stress due to torsion τTA = τ TB = M.rA/J.. and ..τTC = τ TD = M.rC/J τ TA = 5,94.105Nmm.43,9mm / 4,69.105mm4=55,6 N/mm2 τ TC = τTD = 5,945Nmm.31,34mm / 4,69.105mm4= 39,69N/mm2 10) The resultant stresses τ RA, = τ RB and τ RA, =  τ RB are obtained by adding the stress vectors graphically as shown below τRA = τ RB=48,59 N/mm2 τRC = τRD = 45,56N/mm2

Note: The example above simply illustrates the vector method adding direct and torsional shear stresses and compares the difference in using the unit weld width method and using real weld sizes. The example calculates the stress levels in an existing weld group it is clear that the weld is oversized for the loading scenario. The difference in the resulting values are in less than 4%. If the welds were smaller i.e 3mm then the differences would be even smaller.

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Table Properties of Fillet Weld Groups with Welds Treated as Lines

The following table gives the geometric properties of common fillet weld groups where welds are treated as line elements. These weld group properties are widely used in structural engineering, welded connection design, torsional weld analysis, and fillet weld strength calculations.

The table includes weld throat area, centroid location, second moment of area (I_xx), and polar moment of inertia (J) for commonly used weld group configurations.

Weld Geometry	Throat Area Unit Area	Location of Centre of Gravity (COG) x y	Second Moment of Area Ixx (Unit)	Polar Moment of Inertia J (Unit)
	0.707 h d d	x̄ = 0 ȳ = d / 2	Ixx = d³ / 12	J = d³ / 12
	1.414 h d 2 d	x̄ = b / 2 ȳ = d / 2	Ixx = d³ / 6	J = d (3b² + d²) / 6
	1.414 h b 2 b	x̄ = b / 2 ȳ = d / 2	Ixx = b d² / 2	J = b (3d² + b²) / 6
	0.707 h (b + d) b + d	x̄ = b² / 2(b + d) ȳ = d² / 2(b + d)	-	J = ((b + d)⁴ − 6 b² d²) / 12(b + d)
	0.707 h (2b + d) 2b + d	x̄ = b² / (2b + d) ȳ = d / 2	Ixx = d² (6b + d) / 12	z = 8b³ + 6b²d + d³ J = z / 12 − b⁴ / (2b + d)
	1.414 h (b + d) 2(b + d)	x̄ = b / 2 ȳ = d / 2	Ixx = d² (3b + d) / 6	J = (b + d)³ / 6
	1.414 π h r 2 π r	-	I = π r³	J = 2 π r³

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Table Of Weld Capacities

The fillet weld capacity tables related to the type of loading on the weld.  Two types of loading are identified traverse loading and longitudinal loading as show below

The weld loading should be such that

{ (F_L/P_L) ² + (F_T/P_T) ² } ≤ 1

The following table is in accord with data in BS 5950 part 1. Based on design strengths as shown in table below ... Design Strength

P_L = a.p_w
P_T = a.K.p_w

a = weld throat size.

K =1,25 √ (1,5 / (1 + Cos ² θ )

P_T based on elements transmitting forces at 90_o i.e θ = 45_o and K = 1,25

Weld Capacity E35 Electrode S275 Steel					Weld Capacity E42 Electrode S355 Steel
Leg Length	Throat Thickness	Longitudinal Capacity	Transverse Capacity		Leg Length	Throat Thickness	Longitudinal Capacity	Transverse Capacity
		P L(kN/mm)	P T (kN/mm)				P L	P T
mm	mm	kN/mm	kN/mm		mm	mm	kN/mm	kN/mm
3	2,1	0,462	0,577		3	2,1	0,525	0,656
4	2,8	0,616	0,720		4	2,8	0,700	0,875
5	3,5	0,770	0,963		5	3,5	0,875	1,094
6	4,2	0,924	1,155		6	4,2	1,050	1,312
8	5,6	1,232	1,540		8	5,6	1,400	1,750
10	7,0	1,540	1,925		10	7,0	1,750	2,188
12	8,4	1,848	2,310		12	8,4	2,100	2,625
15	10,5	2,310	2,888		15	10,5	2,625	3,281
18	12,6	2,772	3,465		18	12,6	3,150	3,938
20	14,0	3,08	3,850		20	14,0	3,500	4,375
22	15,4	3,388	4,235		22	15,4	3,850	4,813
25	17,5	3,850	4,813		25	17,5	4,375	5,469

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Design Strength p _w of fillet welds

	Electrode classification
Steel Grade	35	43	50
	N/mm2	N/mm2	N/mm2
S275	220	220	220
S355	220	250	250
S460	220	250	280

Related Weld Calculators

The following interactive calculators are available for the weld formulae and weld group properties shown on this page.

Calculator	Use
Fillet Weld Strength & Size Calculator	Calculate fillet weld throat area, weld shear stress, utilisation and required weld size for direct shear loading.
Weld Throat Area Calculator	Calculate effective throat thickness, area of one weld and total effective throat area.
Rectangular Weld Group Properties Calculator	Calculate weld length, throat area, centroid, Ixx, Iyy and polar moment for closed rectangular weld groups.
Rectangular Weld Group Stress Calculator	Calculate rectangular weld group direct shear stress, torsional shear stress, maximum resultant stress and utilisation.
Circular Weld Group Properties Calculator	Calculate circular weld length, effective throat area, centroid and polar moment of inertia.
Circular Weld Group Stress Calculator	Calculate circular weld group direct shear stress, torsional shear stress, maximum resultant stress and utilisation.

Applications of Weld Strength Calculations

• Structural steel design and fabrication
• Mechanical component design
• Pressure vessels and piping systems
• Construction and civil engineering
• Heavy machinery and industrial equipment

Advantages of Welded Joints

• High strength and rigidity
• Efficient load transfer
• No need for additional fasteners
• Suitable for complex geometries
• Permanent and compact connections

Limitations of Welded Joints

• Requires skilled workmanship
• Inspection and quality control needed
• Residual stresses and distortion
• Not easily disassembled
• Fatigue and cracking risks under cyclic loads

Summary of Weld Design Principles

• Use appropriate safety factors (typically 3–5)
• Minimise weld size while meeting strength requirements
• Avoid loading welds directly where possible
• Consider fatigue for cyclic loading
• Follow relevant standards for final design

Frequently Asked Questions

What determines weld strength?

Weld strength depends on weld size, material properties, loading type and joint geometry.

What is the difference between fillet and butt welds?

Fillet welds join surfaces at an angle, while butt welds join components in the same plane.

How are weld stresses calculated?

Weld stresses are calculated using shear and normal stress equations based on applied loads and weld geometry.

What is weld throat thickness?

It is the effective thickness of a weld used in strength calculations.

Why is a safety factor used in weld design?

Safety factors account for uncertainties in loading, materials and workmanship.

Which standard is used for weld design?

BS 5950 and Eurocode 3 (EN 1993) are commonly used standards.

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