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Solution Manual Metal Forming Mechanics and Metallurgy 4th edition(

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Solution Manual Metal Forming Mechanics and Metallurgy 4th edition Solution Manual Metal Forming Mechanics and Metallurgy 4th edition Solution Manual Metal Forming Mechanics and Metallurgy 4th edition Solution Manual Metal Forming Mechanics and Metallurgy 4th edition Solution Manual Metal Forming Mechanics and Metallurgy 4th edition Solution Manual Metal Forming Mechanics and Metallurgy 4th edition Solution Manual Metal Forming Mechanics and Metallurgy 4th edition

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AllChaptersCovered
z z




SOLUTIONMANUAL
z

, Solution Manual3rd Ed. MetalForming: Mechanics and Metallurgy z z z z z z z z




Chapter 1 z z




Determine the principal stresses for the stress state z z z z z z z




10 –3 4
σij = –3 5 2 .
z
z
z z




4 2 7
Solution: I1 = 10+5+7=32, I2 = -(50+35+70) +9 +4 +16 = -126, I3 = 350 -48 -40 -80 z z z z z z z z z z z z z z z z




-63 = 119; σ – 22σ2 -126σ -119 = 0. A trial and error solution gives σ -= 13.04.
3
z z z z z z z z z z z z z z z z z z z




◻ Factoring out 13.04, σ2 -8.96σ + 9.16 = 0. Solving; σ1 = 13.04, σ2 = 7.785, σ3 =
z z z z z z z z z z z z z z z z




1.175.
z




1-2 A 5-cm. diameter solid shaft is simultaneously subjected to an axial load of 80 kN and a
z z z z z z z z z z z z z z z z




torque of 400 Nm.
z z z z




a. Determine the principal stresses at the surface assuming elastic behavior. z z z z z z z z z




b. Find the largest shear stress. z z z z




Solution: a. The shear stress, τ, at a radius, r, is τ = τsr/R where τsis theshearstress at the surface
z z z z z z z z z z z z z z z z z z z z z




R is the radius of the rod. The torque, T, is given by T = ∫2πtr2dr = (2πτs /R)∫r3dr
z z z z z z z z z z z z z z z z z z z




= πτsR3/2. Solving for = τs, τs = 2T/(πR3) = 2(400N)/(π0.0253) = 16 MPa The
z z z z z z z z z z z z z z




axial stress is .08MN/(π0.0252) = 4.07 MPa
z z z z z z z




σ1,σ2 = 4.07/2 ± [(4.07/2)2 + (16/2)2)]1/2 = 1.029, -0.622 MPa
z z z z z z z z z z




b. the largest shear stress is (1.229 + 0.622)/2 = 0.925 MPa
z z z z z z z z z z z




A long thin-wall tube, capped on both ends is subjected to internal pressure. During elastic
z z z z z z z z z z z z z z




loading, does the tube length increase, decrease or remain constant?
z z z z z z z z z z




Solution: Let y= hoop direction, x = axial direction, and z = radial direction. – ex = e2
z z z z z z z z z z z z z z z z
z
z




= (1/E)[σ - v( σ3 + σ1)] = (1/E)[σ2 - v(2σ2)] = (σ2/E)(1-2v)
z
z z z z
z
z z z
z
z z z




Since u < 1/2 for metals, ex = e2 is positive and the tube lengthens.
z z z z z z
z
z
z
z z z z z




4 A solid 2-cm. diameter rod is subjected to a tensile force of 40 kN. An identical rod is
z z z z z z z z z z z z z z z z z




subjected to a fluid pressure of 35 MPa and then to a tensile force of 40 kN. Which rod
z z z z z z z z z z z z z z z z z z z




experiences the largest shear stress?
z z z z z




Solution: The shear stresses in both are identical because a hydrostatic pressure has no shear
z z z z z z z z z z z z z z




component.
z




1-5 Consider a long thin-wall, 5 cm in diameter tube, with a wall thickness of 0.25 mm z z z z z z z z z z z z z z z




that is capped on both ends. Find the three principal stresses when it is loaded under a tensile
z z z z z z z z z z z z z z z z z z




force of 40 N and an internal pressure of 200 kPa.
z z z z z z z z z z z




Solution: σx = PD/4t + F/(πDt) = 12.2 MPa z z z z z z z z




σy = PD/2t = 2.0 MPa z z z z z




σy = 0 z z




1

,1-6 Three strain gauges are mounted on the surface of a part. Gauge A is parallel to the x- z z z z z z z z z z z z z z z z z




axis and gauge C is parallel to the y-axis. The third gage, B, is at 30° to gauge A. When the
z z z z z z z z z z z z z z z z z z z z




part is loaded the gauges read
z z z z z z




Gauge A 3000x10-6 z




Gauge B 3500 x10-6 z z




Gauge C 1000 x10-6 z z




a. Find the value of γxy. z z z z




b. Find the principal strains in the plane of the surface. z z z z z z z z z




c. Sketch the Mohr’s circle diagram. z z z z




Solution: Let the B gauge be on the x’ axis, the A gauge on the x-axis and the C gauge on
z z z z z z z z z z z z z z z z z z z z


2 2
they-axis. ex x =exxℓ x x +e ℓ x y +γxyℓx yyxℓx y, where ℓx x =cosex = 30=√3/2and ℓx y=
z z z z z z z z z z z z z z z z
z
z z z z z z z z z




cos 60 = ½. Substituting the measured strains, 3500 =
z z z z z z z z z




3000(√2/3)2 – 1000(1/2)2 + γxy(√3/2)(1/2)
z z z z z


2 2 -6
γ◻xy=(4/√3/2){3500-[3000–(1000(√3/2) +1 000(1/2) ]} =2,309(x10 )
z z z z z



1/2 2
b. e1,e2 = (ex +ey)/2± [(ex-ey)2 + γxy2]
z z /2 = (3000+1000)/2 ± [(3000-1000) +
z z z z z z z z z z




23092]1/2/2.e1 = 3530(x10-6), e2 = 470(x10-6), e3 = 0. z z z z z z z z z




c)
γ/2
sx



s2 s1
s
sx’

sy



Find the principal stresses in the part of problem 1-6 if the elastic modulus ofthe part is 205
z z z z z z z z z z z z z z z z z z




GPa and Poissons’s ratio is 0.29.
z z z z z z




Solution: e3 = 0 = (1/E)[0- v(σ1+σ2)], σ1= σ2 z z z z z z z z z z z




e1 = (1/E)(σ1 - v σ1); σ1 = Ee1/(1-v) = 205x109(3530x10-6)/(1-.292) = 79 MPa
z z z z z z z z z z z z z




1
Show that the true strain after elongation may be expressed as s =ln(
z z z z z z z z z z z z z z
) where r is the
1–r
z z z z



z z



1
reduction of area. s =ln( ).
z


z z z z z z




1–r z z




Solution: r = (Ao-A1)/Ao =1 – A1/Ao = 1 – Lo/L1. s = ln[1/(1-r)]

z z z z z z z z z z z z z




A thin sheet of steel, 1-mm thick, is bent as described in Example 1-11. Assuming that E
z z z z z z z z z z z z z z z z




=is205 GPaand v=0.29,p=2.0 mandthattheneutralaxis doesn’t shift.
z z z z z z z z z z z z z z z z z




a. Find the state of stress on most of the outer surface. z z z z z z z z z z




b. Find the state of stress at the edge of the outer surface. z z z z z z z z z z z




2

, Solution: a. Substituting E = 205x109, t = 0.001, p = 2.0 and v = 0.29 z z z z z z z z z z z z z z z




Et vEt
intoσx = and σy = ,σx=56MPa,,σy=16.2MPa
2p(1–v )2
z z




2p(1–v2)
z
z z z z z z z z z z
z
z z z z z
z z z z




vEt
b. Now σy = 0, so σy =
z = 51 MPa z z z z z z z z



2p

1-10 For an aluminum sheet, under plane stress loading sx = 0.003 and sy = 0.001. z z z z z z z z z z z z z z




Assumin gthatE=is68GPaand v=0.30,find sz. z z z z z z z z z z z z




Solution: ey = (1/E)(σy-vσy), ex = (1/E)(σx – vEey – v2σx). Solving for σx, z z z z z z z z z z z z z




σx = [E/(1-v2)]ey+ vey). Similarly, σy = [E/(1-v2)](ey+ vex). Substituting into
z z z z z z z z z z z z




ez = (1/E)(-vσy-vσy) = (-v /E)(E/(1-v2)[ey+ vey+ ey+ vex ) = [-v(1+v)//(1-v2)](ey+ey) = 0.29(-
z z z z z z z z z z z z z z z z z




1.29/0.916)(0.004) = -0.00163 z z




1-11 A piece of steel is elastically loaded under principal stresses, σ1 = 300 MPa, σ2 = 250z z z z z z z z z z z z z z z z




MPa and σ3 = -200 MPa. Assuming that E = is 205 GPa and v = 0.29 find the stored elastic
z z z z z z z z z z z z z z z z z z z z z




energy per volume.
z z z




Solution: w = (1/2)(σ1e1 + σ2e2 + σ3e3). Substituting e1 = (1/E)[σ1 - v(σ2 + σ3)], e2 = z z z z z z z z z z z z z z z z z




(1/E)[σ2 - v(σ3 + σ1)] and e3 = (1/E)[σ3 - v(σ1 + σ2)],
w = 1/(2E)[σ 2 + σ 2 + σ 2 - 2v(σ σ +σ σ +σ σ )] =
z z z z z z z z z z z z z



z z z z z z z z z z z z z z z z z z


1 2 3 2 z 3 3 z 1 1 z 2
(1/(2x205x10 )[300 +250 + 200 –(2x0.29)(-200x250 – 300x250 + 250+300)]x1012 = 9 2
z
2
z z
2
z z z z z z




400J/m3
z




1-12 A slab of metal is subjected to plane-strain deformation (e2=0) such that σ1= 40 ksi z z z z z z z z z z z z z z z




and σ3 = 0. Assume that the loading is elastic and z z z z z z z z z z z




that E = is 205 GPa and v = 0.29 (Note the mixed units.) Find
z z z z z z z z z z z z z z




a. the three normal strains. z z z




b. the strain energy per volume. z z z z




Solution: w = (1/2)(σ1e1 + σ2e2 + σ3e3) = (1/2)(σ1e1 + 0 + 0) = σ1e1/2 σ1 = z z z z z z z z z z z z z z z z z




40ksi(6.89MPa/ksi) = 276 MPa
z z z z




0 = e2 = (1/E)[σ2 -v σ1], σ2 =v σ1= 0.29x276 = 80 MPa
z z z z z z z z z z z z z z




e1 = (1/E)(σ1 -v σ2) =(1/205x103)[276-.29(80)] = 0.00121 w
z z z z z z z z




= (276x106)(0.00121)/2 = 167 kJ/m3
z z z z z




Chapter 2 z




a) If the principal stresses on a material with a yield stress in shear of 200 MPa are σ2
z z z z z z z z z z z z z z z z z




= 175 MPa and σ1 = 350 MPa., what is the stress, σ3, at yielding according to the Tresca
z z z z z z z z z z z z z z z z z z




criterion?
z




b) If the stresses in (a) were compressive, what tensile stress σ3 must be applied to cause
z z z z z z z z z z z z z z z




yielding according to the Tresca criterion?
z z z z z z




Solution: a) σ1 - σ3 = 2k, σ3 = 2k – σ1 = 400 - 350 = 50 MPa. z z z z z z z z z z z z z z z z z z




3

Libro relacionado
 image
William F. Hosford, Robert M. Caddell Metal Forming
Editorial: 2011 ISBN: 9781139497435 Edición: Desconocido

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