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A seminar on, 
“Shear Centre” 
Prepared by, 
M.prasannakumar 
Venkatesha.A 
(1RV13CSE06) 
Under the guidance of, 
M.V.Renuka devi 
Professor 
Dept. of Civil Engineering, RVCE, Bangalore 
Classified - Internal use
Introduction 
• Most examples of beam bending involve 
beams with the symmetric cross sections. 
• However, there are an ever increasing number 
of cases where the cross section of a beam is 
not symmetric about any axis. 
• If the cross section of the beam does not have a 
plane of symmetry, the displacements of the 
beam get increasingly complicated. 
Classified - Internal use
Fig.1 Effect of loading at shear center 
Classified - Internal use
Effect of loading at shear center 
• Case1: The displacement consists of both 
translation down and anticlockwise twist. 
• Case2: The displacement consists of both 
translation down and clockwise twist. 
• Somewhere in-between these two extremes we 
would expect a point that we could apply the 
load and produce only a twisting .This point is 
called “shear center” . 
Classified - Internal use
Fig. 2. Effects of loads on unsymmetrical section. 
Classified - Internal use
Effect of loading at shear center 
• The flexural formula σ=My/I is valid only if the 
transverse loads which give rise to bending act in 
a plane of symmetry of beam cross section. 
• In this type of loading there is obviously no 
torsion of the beam. 
• In more general cases the beam cross section will 
have no axis of symmetry and the problem of 
where to apply the load so that the action is 
entirely bending with no torsion arises . 
Classified - Internal use
Advantages of loading the beam at 
the shear center 
• The path of any deflection is more obvious. 
• The beam translates only straight downward. 
The standard deflection formulas can be used 
to calculate the amount of deflection. 
• The flexural formula can be used to calculate 
the stress in the beam. 
Classified - Internal use
Shear Center for Axis Symmetry 
• Every elastic beam cross-section has a point 
through which transverse forces may be 
applied so as to produce bending only, with no 
torsion of the beam. The point is called the 
“shear center” of the beam. 
• The shear center for any transverse section of 
the beam is the point of intersection of the 
bending axis and the lane of the transverse 
section. Shear center is also called center of 
twist. 
Classified - Internal use
Flexure axis or bending axis 
• Flexural axis of a beam is the longitudinal axis 
through which the transverse bending loads must 
pass in order that the bending of the beam shall 
not be accompanied by twisting of the beam. 
• In Fig.3 ABCD is a plane containing the principal 
centroidal axis of inertia and plane AB’C’D is the 
plane containing the loads. These loads will cause 
unsymmetrical bending. In Fig.3 AD is the flexural 
axis [2]. 
Classified - Internal use
Fig.3 Flexural axis or bending axis 
Classified - Internal use
Classification on the basis of symmetry 
• Double symmetrical section 
• Single symmetrical section 
• Unsymmetrical section 
Classified - Internal use
Fig.4 Two axis symmetry[7] 
Classified - Internal use
Fig.5 One axis symmetry & unsymmetrical section[7] 
Classified - Internal use
Shear center or Center of flexure 
• Beam carries loads which are transverse to the 
axis of the beam and which cause not only 
normal stresses due to flexure but also 
transverse shear stresses in any section. 
• Consider the cantilever beam shown in Fig.7 
carrying a load at the free end. In general, this 
will cause both bending and twisting. 
Classified - Internal use
Fig. 6 Cantilever beam loaded with force P 
Classified - Internal use
Shear center or Center of flexure 
• Let Ox be centroidal axis .The load, in general will, 
at any section, cause: 
1. Normal stress 휎푥 due to flexure; 
2. Shear stresses 휏푥푦 and 휏푥푧 due to the 
transverse nature of the loading; and 
3. Shear stresses 휏푥푦 and 휏푥푧 due to torsion. 
4. To arrive at the solution, we assume that 
휎푥=- 
−푃 퐿−푥 푦 
퐼푧 
,휎푦=휎푧=휏푦푧=0 
This is known as St.Venant’s assumption. 
Classified - Internal use
Shear center or Center of flexure 
• A position can be established for which no 
rotation occurs . 
• If a transverse force is applied at this point, we 
can resolve it into two components parallel to the 
y and z axis and note from the above discussion 
that these components do not produce the rotation 
of centroidal elements of the cross sections of the 
beam. This point is called the shear center of 
flexure or flexural centre. 
Classified - Internal use
Fig. 7 Load P passing through shear centre 
Classified - Internal use
Shear center for a Channel section 
Fig. 8 Beam of Chanel cross section. 
Classified - Internal use
Shear center for a Channel section 
• F1= (휏a/2) bt , and sum of vertical shear 
stresses over area of web is, 
ℎ/2 
F3= −ℎ/2 
휏 푡 푑푦 
• F1h=Fe and F=F3 
• e = 
퐹1ℎ 
퐹 
= 
1 
2 
휏푎푏1푡ℎ 
퐹 
= 
푏1푡ℎ 
2퐹 
퐹3푄 
퐼푡 
= 
푏1 푡ℎ 퐹3 푏1푡( 
ℎ 
2 
) 
2퐹 .퐼.푡 
e= 
2 
4퐼 
푏1 
ℎ2 푡 
Classified - Internal use
Shear center for a Channel section 
• I= Iweb + 2 Iflange = 
1 
12 
tℎ3 + 2[ (1/12) b1 푡3 + b1 t (h/2)^2 
• =(1/12) t ℎ2 (6b + h) 
• So finally, e= 
3 
6푏푡ℎ 
2 = 
푏1 
푏1 
2+ 
ℎ 
3푏푡 
• Here ‘e’ is independent of the magnitude of applied force F as well 
as of its location along the beam. 
• The shear center for any cross section lies on a longitudinal line 
parallel to the axis of the beam. 
• The procedure of locating the shear center consists of determining 
the shear forces , as F1 and F3 at a section and then finding the 
location of the external forces as F1 and F3,at a section and then 
finding the location of the external force necessary to keep these 
forces in equilibrium. 
Classified - Internal use
Shear center for I-section: 
Fig. 9 Beam of Chanel cross section. 
Classified - Internal use
Shear center for I-section: 
• Assuming an I section of cross-sections mentioned in 
figure, 
• For equilibrium,F1 + F2 =F 
• Likewise to have no twist of the section,From ΣMA=0, 
Fe1 =Fe2h & Fe2= F1h, 
• Since the area of a parabola is (2/3) of the base times 
the maximum altitude. 
• F2= (2/3) b2 (q2) max 
• Since V=F 
• (q2) max= VQ/I =FQ/I 
Classified - Internal use
Shear center for I-section 
• Where Q is the statical moment of the upper half of 
the right hand flange and I is the moment of inertia of 
the whole section. Hence 
• Fe=F2h= (2/3) b2 (q2) max 
• e1= (2hb2Q)/(3I)= (2h b2/3I) (b2 t2 /2 ) (b2/4) = h/I (t2 
3) 
b2 푏2 
• Where I2 is the moment of inertia of the right hand 
flange around the central axis. 
• e2=h ( I1/ I ) 
• Where I1 is the moment of inertia of left hand flange. 
Classified - Internal use
Shear Centers for a few other sections 
• Thin walled inverted T-section, the distribution 
of shear stress due to transverse shear will be 
as shown in Fig.11 . 
• The moment of this distributed stress about C 
is obviously zero. Hence, the shear center for 
this section is C. 
Classified - Internal use
Fig .10. Location of shear centre for inverted T-section 
and angle section. 
Classified - Internal use
Fig.11 Twisting effect on some cross-sections if load is 
not applied through shear center. 
Classified - Internal use
1. Determination of the shear centre for the 
channel section shown in figure below. 
Classified - Internal use
Solution 
• e= 
푏1 
2+ 
푤ℎ 
3푏푡 
• Here b1 =10-1=9cm 
• h =15-1=14cm 
• w =1cm 
• t =1cm 
• e = 
1 
2 
.9 
1+ 
1 
2 
.9 
1 
6 
. 
(1 푋14) 
(9푋 1) 
=3.57 cm 
Classified - Internal use
2.Locating the shear centre of the cross section 
shown in figure. 
Classified - Internal use
Solution 
• H2 = 휏 푑퐴 
= 
퐹퐴푦 
퐼 푡 
퐹 
퐼 푡 
dA = 
퐴 푦 dA 
퐹 
퐼 푡 
= 
3 
2 3 − 푥 6.5 2 푑푥 = 58.5(F/I) 
0 
퐹 
2퐼 
• H1 = 
4 
2 4 − 푥 푋 6.5 푋 2푑푥 =104(F/I) 
0 
• Taking moments about point D, we get 
• FR e = 2 (H1 –H2) 6.5 
• =2(104-58.5)6.5 X (F/I) 
• Now FR= F 
2푋 45.5 푋 6.5 
• e = 
퐼 
=591.5/I 
• I = 2[ 
7푋23 
12 
+ 14 X 6.52 ]+ 
1푋113 
12 
• =1303.251 푐푚4 
• e = 591.5 / 1303.251 = 0.454 cm 
Classified - Internal use
3.Determination of shear centre for a circular open 
section 
Classified - Internal use
Solution 
• The static moment of the crossed section is, 
휃 
Qz = 0 
푅 푑휑 푡 푅 푠푖푛휑 
• =R^2 . t (1-cos휃) 
• Iyz=0, 
• 휏푥푧 = 퐹 
푄푧 
푡퐼푧 
= ( F/t Iz ) R^2 t (1-cos휃 ) 
• But Iz = 휋. R^3. T 
• Hence휏푥푧 = 
퐹 
휋푅푡 
(1 − 푐표푠휃) 
• When 휃 = 180°, 
• 휏푥푧 = 2F / (휋푅푡) 
2휋 
• M= 0 
휏푥푧 푅푑휃 푡 푅 
• = 
퐹 
휋푅푡 
2휋 
0 
푅2 푡 (1 − cos 휃 ) 푑휃 
• = 2 FR 
Classified - Internal use
Conclusion 
• The shear center is having practical significance 
in the study of behavior of beams with section 
comprising of thin parts, such as channels, angles, 
I-sections, which are having less resistance to 
torsion but high resistance to flexure. 
• To prevent twisting of any beam cross-section, the 
load must be applied through the shear centre. 
• It is not necessary, in general, for the shear centre 
to lie on the principal axis, and it may be located 
outside the cross section of the beam. 
Classified - Internal use
References 
1. Alok Gupta (2004) , “Advanced strength of materials’’, Umesh 
Publications, First Edition. 
2. LS Srinath, “Advanced Mechanics of solids”, 15th edition, Tata McGraw 
Hill. 
3. Timoshenko & JN Goodier (1997), “Mechanics of solids”, Tata McGraw 
Hill. 
4. S.S.Bhavikatti,“Structural Analysis” ,Vol.2. 
5. Vazrani and Ratwani“ Analysis of structures”,Vol 2. 
6. B.C.Punmia & A.K.Jain . “Strength of materials and Theory of 
structures”, Vol.2Laxmi Publications (P) Ltd. 
7. James Gere & Barry Goodno, “ Mechanics of materials”, Google Books. 
8. A.C. Ugral ,“Advanced Mechanics of Materials and Applied 
Elasticity”,Fifth Edition”, Safari Books Online. 
9. http://gaia.ecs.csus.edu/-ce113/steel -shear.pdf 
10. http://www.me.mtu.edu/-mavable/Spring03/chap6.pdf 
11. Jaehong Lee, “Centre of gravity and shear centre”, 
www.elsevier.com/locate/compstruct. 
Classified - Internal use

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shear centre

  • 1. A seminar on, “Shear Centre” Prepared by, M.prasannakumar Venkatesha.A (1RV13CSE06) Under the guidance of, M.V.Renuka devi Professor Dept. of Civil Engineering, RVCE, Bangalore Classified - Internal use
  • 2. Introduction • Most examples of beam bending involve beams with the symmetric cross sections. • However, there are an ever increasing number of cases where the cross section of a beam is not symmetric about any axis. • If the cross section of the beam does not have a plane of symmetry, the displacements of the beam get increasingly complicated. Classified - Internal use
  • 3. Fig.1 Effect of loading at shear center Classified - Internal use
  • 4. Effect of loading at shear center • Case1: The displacement consists of both translation down and anticlockwise twist. • Case2: The displacement consists of both translation down and clockwise twist. • Somewhere in-between these two extremes we would expect a point that we could apply the load and produce only a twisting .This point is called “shear center” . Classified - Internal use
  • 5. Fig. 2. Effects of loads on unsymmetrical section. Classified - Internal use
  • 6. Effect of loading at shear center • The flexural formula σ=My/I is valid only if the transverse loads which give rise to bending act in a plane of symmetry of beam cross section. • In this type of loading there is obviously no torsion of the beam. • In more general cases the beam cross section will have no axis of symmetry and the problem of where to apply the load so that the action is entirely bending with no torsion arises . Classified - Internal use
  • 7. Advantages of loading the beam at the shear center • The path of any deflection is more obvious. • The beam translates only straight downward. The standard deflection formulas can be used to calculate the amount of deflection. • The flexural formula can be used to calculate the stress in the beam. Classified - Internal use
  • 8. Shear Center for Axis Symmetry • Every elastic beam cross-section has a point through which transverse forces may be applied so as to produce bending only, with no torsion of the beam. The point is called the “shear center” of the beam. • The shear center for any transverse section of the beam is the point of intersection of the bending axis and the lane of the transverse section. Shear center is also called center of twist. Classified - Internal use
  • 9. Flexure axis or bending axis • Flexural axis of a beam is the longitudinal axis through which the transverse bending loads must pass in order that the bending of the beam shall not be accompanied by twisting of the beam. • In Fig.3 ABCD is a plane containing the principal centroidal axis of inertia and plane AB’C’D is the plane containing the loads. These loads will cause unsymmetrical bending. In Fig.3 AD is the flexural axis [2]. Classified - Internal use
  • 10. Fig.3 Flexural axis or bending axis Classified - Internal use
  • 11. Classification on the basis of symmetry • Double symmetrical section • Single symmetrical section • Unsymmetrical section Classified - Internal use
  • 12. Fig.4 Two axis symmetry[7] Classified - Internal use
  • 13. Fig.5 One axis symmetry & unsymmetrical section[7] Classified - Internal use
  • 14. Shear center or Center of flexure • Beam carries loads which are transverse to the axis of the beam and which cause not only normal stresses due to flexure but also transverse shear stresses in any section. • Consider the cantilever beam shown in Fig.7 carrying a load at the free end. In general, this will cause both bending and twisting. Classified - Internal use
  • 15. Fig. 6 Cantilever beam loaded with force P Classified - Internal use
  • 16. Shear center or Center of flexure • Let Ox be centroidal axis .The load, in general will, at any section, cause: 1. Normal stress 휎푥 due to flexure; 2. Shear stresses 휏푥푦 and 휏푥푧 due to the transverse nature of the loading; and 3. Shear stresses 휏푥푦 and 휏푥푧 due to torsion. 4. To arrive at the solution, we assume that 휎푥=- −푃 퐿−푥 푦 퐼푧 ,휎푦=휎푧=휏푦푧=0 This is known as St.Venant’s assumption. Classified - Internal use
  • 17. Shear center or Center of flexure • A position can be established for which no rotation occurs . • If a transverse force is applied at this point, we can resolve it into two components parallel to the y and z axis and note from the above discussion that these components do not produce the rotation of centroidal elements of the cross sections of the beam. This point is called the shear center of flexure or flexural centre. Classified - Internal use
  • 18. Fig. 7 Load P passing through shear centre Classified - Internal use
  • 19. Shear center for a Channel section Fig. 8 Beam of Chanel cross section. Classified - Internal use
  • 20. Shear center for a Channel section • F1= (휏a/2) bt , and sum of vertical shear stresses over area of web is, ℎ/2 F3= −ℎ/2 휏 푡 푑푦 • F1h=Fe and F=F3 • e = 퐹1ℎ 퐹 = 1 2 휏푎푏1푡ℎ 퐹 = 푏1푡ℎ 2퐹 퐹3푄 퐼푡 = 푏1 푡ℎ 퐹3 푏1푡( ℎ 2 ) 2퐹 .퐼.푡 e= 2 4퐼 푏1 ℎ2 푡 Classified - Internal use
  • 21. Shear center for a Channel section • I= Iweb + 2 Iflange = 1 12 tℎ3 + 2[ (1/12) b1 푡3 + b1 t (h/2)^2 • =(1/12) t ℎ2 (6b + h) • So finally, e= 3 6푏푡ℎ 2 = 푏1 푏1 2+ ℎ 3푏푡 • Here ‘e’ is independent of the magnitude of applied force F as well as of its location along the beam. • The shear center for any cross section lies on a longitudinal line parallel to the axis of the beam. • The procedure of locating the shear center consists of determining the shear forces , as F1 and F3 at a section and then finding the location of the external forces as F1 and F3,at a section and then finding the location of the external force necessary to keep these forces in equilibrium. Classified - Internal use
  • 22. Shear center for I-section: Fig. 9 Beam of Chanel cross section. Classified - Internal use
  • 23. Shear center for I-section: • Assuming an I section of cross-sections mentioned in figure, • For equilibrium,F1 + F2 =F • Likewise to have no twist of the section,From ΣMA=0, Fe1 =Fe2h & Fe2= F1h, • Since the area of a parabola is (2/3) of the base times the maximum altitude. • F2= (2/3) b2 (q2) max • Since V=F • (q2) max= VQ/I =FQ/I Classified - Internal use
  • 24. Shear center for I-section • Where Q is the statical moment of the upper half of the right hand flange and I is the moment of inertia of the whole section. Hence • Fe=F2h= (2/3) b2 (q2) max • e1= (2hb2Q)/(3I)= (2h b2/3I) (b2 t2 /2 ) (b2/4) = h/I (t2 3) b2 푏2 • Where I2 is the moment of inertia of the right hand flange around the central axis. • e2=h ( I1/ I ) • Where I1 is the moment of inertia of left hand flange. Classified - Internal use
  • 25. Shear Centers for a few other sections • Thin walled inverted T-section, the distribution of shear stress due to transverse shear will be as shown in Fig.11 . • The moment of this distributed stress about C is obviously zero. Hence, the shear center for this section is C. Classified - Internal use
  • 26. Fig .10. Location of shear centre for inverted T-section and angle section. Classified - Internal use
  • 27. Fig.11 Twisting effect on some cross-sections if load is not applied through shear center. Classified - Internal use
  • 28. 1. Determination of the shear centre for the channel section shown in figure below. Classified - Internal use
  • 29. Solution • e= 푏1 2+ 푤ℎ 3푏푡 • Here b1 =10-1=9cm • h =15-1=14cm • w =1cm • t =1cm • e = 1 2 .9 1+ 1 2 .9 1 6 . (1 푋14) (9푋 1) =3.57 cm Classified - Internal use
  • 30. 2.Locating the shear centre of the cross section shown in figure. Classified - Internal use
  • 31. Solution • H2 = 휏 푑퐴 = 퐹퐴푦 퐼 푡 퐹 퐼 푡 dA = 퐴 푦 dA 퐹 퐼 푡 = 3 2 3 − 푥 6.5 2 푑푥 = 58.5(F/I) 0 퐹 2퐼 • H1 = 4 2 4 − 푥 푋 6.5 푋 2푑푥 =104(F/I) 0 • Taking moments about point D, we get • FR e = 2 (H1 –H2) 6.5 • =2(104-58.5)6.5 X (F/I) • Now FR= F 2푋 45.5 푋 6.5 • e = 퐼 =591.5/I • I = 2[ 7푋23 12 + 14 X 6.52 ]+ 1푋113 12 • =1303.251 푐푚4 • e = 591.5 / 1303.251 = 0.454 cm Classified - Internal use
  • 32. 3.Determination of shear centre for a circular open section Classified - Internal use
  • 33. Solution • The static moment of the crossed section is, 휃 Qz = 0 푅 푑휑 푡 푅 푠푖푛휑 • =R^2 . t (1-cos휃) • Iyz=0, • 휏푥푧 = 퐹 푄푧 푡퐼푧 = ( F/t Iz ) R^2 t (1-cos휃 ) • But Iz = 휋. R^3. T • Hence휏푥푧 = 퐹 휋푅푡 (1 − 푐표푠휃) • When 휃 = 180°, • 휏푥푧 = 2F / (휋푅푡) 2휋 • M= 0 휏푥푧 푅푑휃 푡 푅 • = 퐹 휋푅푡 2휋 0 푅2 푡 (1 − cos 휃 ) 푑휃 • = 2 FR Classified - Internal use
  • 34. Conclusion • The shear center is having practical significance in the study of behavior of beams with section comprising of thin parts, such as channels, angles, I-sections, which are having less resistance to torsion but high resistance to flexure. • To prevent twisting of any beam cross-section, the load must be applied through the shear centre. • It is not necessary, in general, for the shear centre to lie on the principal axis, and it may be located outside the cross section of the beam. Classified - Internal use
  • 35. References 1. Alok Gupta (2004) , “Advanced strength of materials’’, Umesh Publications, First Edition. 2. LS Srinath, “Advanced Mechanics of solids”, 15th edition, Tata McGraw Hill. 3. Timoshenko & JN Goodier (1997), “Mechanics of solids”, Tata McGraw Hill. 4. S.S.Bhavikatti,“Structural Analysis” ,Vol.2. 5. Vazrani and Ratwani“ Analysis of structures”,Vol 2. 6. B.C.Punmia & A.K.Jain . “Strength of materials and Theory of structures”, Vol.2Laxmi Publications (P) Ltd. 7. James Gere & Barry Goodno, “ Mechanics of materials”, Google Books. 8. A.C. Ugral ,“Advanced Mechanics of Materials and Applied Elasticity”,Fifth Edition”, Safari Books Online. 9. http://gaia.ecs.csus.edu/-ce113/steel -shear.pdf 10. http://www.me.mtu.edu/-mavable/Spring03/chap6.pdf 11. Jaehong Lee, “Centre of gravity and shear centre”, www.elsevier.com/locate/compstruct. Classified - Internal use