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Torsion

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Cylindrical shafts. Compatibility: relation between shear strain g and angle of twist b. ... acting on sub-section i. Since twist of all sub-sections is the ... – PowerPoint PPT presentation

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Title: Torsion


1
Torsion
  • Cylindrical shafts
  • Compatibility relation between shear strain g
    and angle of twist b.
  • Lg rb ? g (b/L)r (1)
  • Elasticity relation between shear stress t and
    shear strain g.
  • t Gg (Gb/L)r (2)
  • Equilibrium relation between applied torque and
    internal shear stress distribution

2
Torsion
  • Internal shear stress distribution is equivalent
    to the torque

where J is the torsion constant (equal to the
polar moment of area in this special case)
  • Eliminating b between Eq. (2) and Eq. (3)
  • Strength constant

3
Torsion
  • Bars with non-circular cross section
  • z axis of twist
  • q angle of twist per unit length
  • b qz
  • Displacement components
  • u qyz, v qxz, w qy(x,y)
  • y(x,y) warping function

4
Torsion
Shear strain
Solution for stress Compatibility equation
Equilibrium equation
Prandtls stress function f
Equilibrium equation identically satisfied while
compatibility equation becomes
5
Torsion
  • Boundary condition no traction on lateral
    surface S
  • sPz szx cosg szy sing 0 on S
  • This leads to
  • f 0 on S
  • Torque

With the stresses found as functions of x, y and
q, the above integral is reduced to the form
Thus the integration of r.h.s. of (4) produces
the torsional constant J.
6
TorsionSolutions for the stress function
  • Elliptical section
  • Assumed solution
  • This satisfies the boundary condition. It also
    satisfies the differential equation if B is given
    by
  • Stresses

7
TorsionSolutions for the stress function
  • Elliptical section
  • Maximum shear stress
  • Torsional constant
  • Strength constant (defined through T Ctmax)

8
TorsionSolutions for the stress function
  • Equilateral triangle section
  • Assumed solution
  • This satisfies the boundary condition. It also
    satisfies the differential equation if B is given
    by
  • Maximum shear stress
  • Torsion constant
  • Strength constant

9
Torsion Rectangular section
  • Series solution for the stresses valid for b ? h
    leads to
  • tmax szy( h,0) k3(2h)Gq (5)
  • With only the first term in the series retained
  • Substituting the stresses into the integral
    giving the torque

10
Torsion Rectangular section
  • Again, sufficient accuracy is achieved by
    retaining the first term in the series (n 0)
  • T ? k1 (2b)(2h)3Gq (6)

where
  • From (5) and (6)
  • T ? k2 (2b)(2h)2 tmax, k2 k1/k3
  • ? Torsional constant J k1 (2b)(2h)3
  • Strength constant C k2 (2b)(2h)2

11
Torsion composite section
  • The section is divided into N sub-sections of
    known torsional properties.
  • Total torque

where Ti is the torque acting on sub-section i.
Since twist of all sub-sections is the same,
  • Section made up of rectangular sections
  • Ti Ci (tmax)I
  • Hence

12
Torsion composite section examples
  • Open channel section (all dimensions in mm)
  • Find tmax due to T 600 Nm
  • 2h1 9, 2b1 100
  • 2h2 5, 2b2 182
  • 2h3 9, 2b3 100
  • Since bi/hi gt 10 for all i
  • k1 ? k2 ? 0.333, k3 ? 1

where ? tmax 96.11 MPa
13
Torsion composite section examples
  • Open I-section (all dimensions in mm)
  • Determine T for an allowable shear stress of 240
    MPa and a safety factor of 3
  • 2h1 2h2 2h3 2h 6,
  • 2b1 2b3 100, 2b2 138
  • bi/hi gt 10 for all i
  • k1 ? k2 ? 0.333, k3 ? 1

where
? T 324.5 Nm
14
Torsion closed thin-wall section
  • Relative to a curvilinear frame of reference s-n
  • szn ? 0, szs t(s)
  • Equilibrium in z direction gives
  • Shear flow q(s) t(s) t(s) constant.
  • Torque
  • where A is the area enclosed by the centreline
    l.
  • Strain energy must be equal to the work done by
    the torque

Substituting from (Eq. 7) to Eq. (8)
15
Torsion closed section with internal walls
  • Section considered as an assembly of N tubular
    sub-sections (compartments), each subjected to
    torque Ti.
  • Total torque

Compartment i
Common twist for all compartments
where q? is the shear flow due to torque in
adjacent compartments.
16
Torsion closed section with internal walls
  • Example 6.6
  • Determine maximum torque for an allowable shear
    stress of 40 MPa.
  • G 26 GPa

T T1 T2 2A1q1 2A2q2 A1 (60?103)2, A2
0.5p(30?103)2
  • ? q1 / q2 1.22 BUT t1 / t2 1.5
  • Therefore maximum shear develops in l2
  • q2 t2tmax 120?103, q1 1.22 q2 ? max T
  • For the wall with t3 1.5, check that (q1
    q2)/1.5 lt tmax
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