CHAPTER 7 MECHANICAL PROPERTIES PROBLEM SOLUTIONS PDF

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CHAPTER 7 MECHANICAL PROPERTIES PROBLEM SOLUTIONS Concepts of Stress and Strain 7.1 (a) Equations 7.4a and 7.4b are expressions for normal (σ′) and shear (τ′) stresses, respectively, as a function of the applied tensile stress (σ) and the inclination angle of the plane on which these stresses are ta...

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CHAPTER 7

MECHANICAL PROPERTIES PROBLEM SOLUTIONS

Concepts of Stress and Strain 7.1 (a) Equations 7.4a and 7.4b are expressions for normal (σ′) and shear (τ′) stresses, respectively, as a function of the applied tensile stress (σ) and the inclination angle of the plane on which these stresses are taken (θ of Figure 7.4). Make a plot on which is presented the orientation parameters of these expressions (i.e., cos2 θ and sin θ cos θ) versus θ. (b) From this plot, at what angle of inclination is the normal stress a maximum? Solution (a) Below are plotted curves of cos2θ (for σ' ) and sin θ cos θ (for τ') versus θ.

(b) The maximum normal stress occurs at an inclination angle of 0°. (c) The maximum shear stress occurs at an inclination angle of 45°. Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful.

Stress-Strain Behavior 7.2 A cylindrical specimen of a nickel alloy having an elastic modulus of 207 GPa (30 × 106 psi) and an original diameter of 10.2 mm (0.40 in.) will experience only elastic deformation when a tensile load of 8900 N (2000 lbf) is applied. Compute the maximum length of the specimen before deformation if the maximum allowable elongation is 0.25 mm (0.010 in.). Solution We are asked to compute the maximum length of a cylindrical nickel specimen (before deformation) that is deformed elastically in tension. For a cylindrical specimen

⎛ d ⎞2 A0 = π⎜ 0 ⎟ ⎝2 ⎠ where d0 is the original diameter. Combining Equations 7.1, 7.2, and 7.5 and solving for l0 leads to

l0 =

=

Δl Δl = Ź= σ ε E

⎛ d ⎞2 Δl Eπ ⎜ 0 ⎟ Δl Eπ d02 Δl E ⎝2 ⎠ Ź= = F F 4F A0

(0.25 × 10−3 m)(207 × 10 9 N / m2 ) (π) (10.2 × 10−3 m) 2 (4)(8900 N)

= 0.475 m = 475 mm (18.7 in.)

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7.3 Consider a cylindrical nickel wire 2.0 mm (0.08 in.) in diameter and 3 × 104 mm (1200 in.) long. Calculate its elongation when a load of 300 N (67 lbf) is applied. Assume that the deformation is totally elastic. Solution In order to compute the elongation of the Ni wire when the 300 N load is applied we must employ Equations 7.1, 7.2, and 7.5. Solving for ∆l and realizing that for Ni, E = 207 GPa (30 x 106 psi) (Table 7.1),

l F σ Δl = l0ε = l0 = 0 = EA0 E

=

(4)(30 m)(300 N)

(207 × 10 9 N / m2 )(π )(2 × 10−3 m) 2

l0F

⎛ d ⎞2 Eπ ⎜ 0 ⎟ ⎝2 ⎠

=

4 l0F

Eπd02

= 0.0138 m = 13.8 mm (0.53 in.)

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7.4 For a brass alloy, the stress at which plastic deformation begins is 345 MPa (50,000 psi), and the modulus of elasticity is 103 GPa (15.0 × 106 psi). (a) What is the maximum load that may be applied to a specimen with a cross-sectional area of 130 mm2 (0.2 in.2) without plastic deformation? (b) If the original specimen length is 76 mm (3.0 in.), what is the maximum length to which it may be stretched without causing plastic deformation?

Solution (a) This portion of the problem calls for a determination of the maximum load that can be applied without plastic deformation (Fy). Taking the yield strength to be 345 MPa, and employment of Equation 7.1 leads to

Fy = σ y A0 = (345 × 106 N/m2 )(130 × 10-6 m2 )

= 44,850 N (10,000 lbf) (b) The maximum length to which the sample may be deformed without plastic deformation is determined from Equations 7.2 and 7.5 as ⎛ σ⎞ li = l0 (1 + ε) = l0 ⎜1 + ⎟ ⎝ E⎠

⎡ 345 MPa ⎤ = (76 mm) ⎢1 + ⎥ = 76.25 mm (3.01 in.) 103 × 103 MPa ⎦ ⎣

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7.5 Consider a cylindrical specimen of a steel alloy (Figure 7.33) 8.5 mm (0.33 in.) in diameter and 80 mm (3.15 in.) long that is pulled in tension. Determine its elongation when a load of 65,250 N (14,500 lbf) is applied.

Solution First it becomes necessary to compute the stress when a load of 65,250 N is applied using Equation 7.1 as

σ =

F = A0

F 2

⎛d ⎞ π⎜ 0 ⎟ ⎝2⎠

=

65,250 N ⎛ 8.5 × 10−3 m ⎞2 π⎜ ⎟ 2 ⎝ ⎠

= 1150 MPa (170, 000 psi)

Referring to Figure 7.33, at this stress level we are in the elastic region on the stress-strain curve, which corresponds to a strain of 0.0054. Now, utilization of Equation 7.2 to compute the value of Δl Δ l = ε l0 = (0.0054)(80 mm) = 0.43 mm (0.017 in.)

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7.6 In Section 2.6 it was noted that the net bonding energy EN between two isolated positive and negative ions is a function of interionic distance r as follows:

EN = −

B A + n r r

(7.30)

where A, B, and n are constants for the particular ion pair. Equation 7.30 is also valid for the bonding energy between adjacent ions in solid materials. The modulus of elasticity E is proportional to the slope of the interionic force–separation curve at the equilibrium interionic separation; that is, ⎛ dF ⎞ E ∝ ⎜ ⎟ ⎝ dr ⎠r

0

Derive an expression for the dependence of the modulus of elasticity on these A, B, and n parameters (for the twoion system) using the following procedure: 1. Establish a relationship for the force F as a function of r, realizing that

F =

dEN dr

2. Now take the derivative dF/dr. 3. Develop an expression for r0, the equilibrium separation. Since r0 corresponds to the value of r at the minimum of the EN-versus-r curve (Figure 2.8b), take the derivative dEN/dr, set it equal to zero, and solve for r, which corresponds to r0. 4. Finally, substitute this expression for r0 into the relationship obtained by taking dF/dr. Solution This problem asks that we derive an expression for the dependence of the modulus of elasticity, E, on the parameters A, B, and n in Equation 7.30. It is first necessary to take dEN/dr in order to obtain an expression for the force F; this is accomplished as follows:

⎛B⎞ ⎛ A⎞ d⎜ ⎟ d ⎜− ⎟ dE N ⎝ r⎠ ⎝ n⎠ F = = + r dr dr dr

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=

A r2

−

nB r (n +1)

The second step is to set this dEN/dr expression equal to zero and then solve for r (= r0). The algebra for this procedure is carried out in Problem 2.9, with the result that ⎛ A ⎞1/(1 − n) r0 = ⎜ ⎟ ⎝ nB ⎠

Next it becomes necessary to take the derivative of the force (dF/dr), which is accomplished as follows: ⎛ A⎞ ⎛ nB ⎞ d⎜ ⎟ d ⎜− ⎟ dF ⎝r2 ⎠ ⎝ r (n +1) ⎠ = + dr dr dr =−

2A r3

+

(n)(n + 1)B r (n + 2)

Now, substitution of the above expression for r0 into this equation yields ⎛ dF ⎞ 2A (n)(n + 1) B + ⎜ ⎟ =− 3/(1− n) ⎝ dr ⎠r ⎛ A⎞ ⎛ A ⎞(n + 2) /(1− n) 0 ⎜ ⎟ ⎜ ⎟ ⎝ nB ⎠ ⎝ nB ⎠

which is the expression to which the modulus of elasticity is proportional.

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7.7 Using the solution to Problem 7.6, rank the magnitudes of the moduli of elasticity for the following hypothetical X, Y, and Z materials from the greatest to the least. The appropriate A, B, and n parameters (Equation 7.30) for these three materials are tabulated below; they yield EN in units of electron volts and r in nanometers:

Material

A

B

X

1.5

7.0 × 10–6

8

2.0

1.0 × 10

–5

9

4.0 × 10

–6

7

Y Z

3.5

n

Solution This problem asks that we rank the magnitudes of the moduli of elasticity of the three hypothetical metals X, Y, and Z. From Problem 7.6, it was shown for materials in which the bonding energy is dependent on the interatomic distance r according to Equation 7.30, that the modulus of elasticity E is proportional to

E ∝−

2A ⎞3/(1− n)

⎛ A ⎜ ⎟ ⎝ nB ⎠

+

(n)(n + 1) B ⎛ A ⎞(n + 2) /(1− n) ⎜ ⎟ ⎝ nB ⎠

For metal X, A = 1.5, B = 7 × 10-6, and n = 8. Therefore, E ∝ −

(8)(8 +1) (7 × 10−6 ) + ⎡ ⎤3 /(1 − 8) ⎡ ⎤(8 + 2) /(1 − 8) 1.5 1.5 ⎢ ⎥ ⎢ ⎥ ⎢ (8) (7 × 10−6 ) ⎥ ⎣ (8) (7 × 10−6 ) ⎦ ⎣ ⎦ (2)(1.5)

= 830 For metal Y, A = 2.0, B = 1 × 10-5, and n = 9. Hence E ∝ −

(2)(2.0) ⎡ ⎢ ⎢ (9) ⎣

3 /(1 − 9)

⎤ 2.0 ⎥ (1 × 10−5 ) ⎥⎦

+

(9)(9 + 1) (1 × 10−5 ) ⎤(9 + 2) /(1 − 9) ⎡ 2.0 ⎥ ⎢ ⎣ (9) (1 × 10−5 ) ⎦

= 683

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And, for metal Z, A = 3.5, B = 4 × 10-6, and n = 7. Thus E ∝ −

(2)(3.5) ⎡ ⎢ ⎢ (7) ⎣

3 /(1 − 7)

⎤ 3.5 ⎥ −6 (4 × 10 ) ⎥⎦

+

(7)(7 + 1) (4 × 10−6 ) ⎤(7 + 2) /(1 − 7) ⎡ 3.5 ⎥ ⎢ ⎣ (7) (4 × 10−6 ) ⎦

= 7425 Therefore, metal Z has the highest modulus of elasticity, followed by metal X, and then metal Y.

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Elastic Properties of Materials 7.8

A cylindrical bar of aluminum 19 mm (0.75 in.) in diameter is to be deformed elastically by

application of a force along the bar axis. Using the data in Table 7.1, determine the force that will produce an elastic reduction of 2.5 × 10–3 mm (1.0 × 10–4 in.) in the diameter.

Solution This problem asks that we calculate the force necessary to produce a reduction in diameter of 2.5×10-3 mm for a cylindrical bar of aluminum. For a cylindrical specimen, the cross-sectional area is equal to

A0 =

π d02 4

Now, combining Equations 7.1 and 7.5 leads to F F = = Eε z A0 πd02

σ =

4

And, since from Equation 7.8 Δd d0

ε Δd =− εz = − x = − ν ν νd0

Substitution of this equation into the above expression gives ⎛ Δd ⎞ ⎟⎟ = E ⎜⎜− πd02 ⎝ νd0 ⎠ 4 F

And, solving for F leads to d Δd π E F = − 0 4ν

From Table 7.1, for aluminum, ν = 0.33 and E = 69 GPa. Thus, Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful.

F = −

(19 × 10−3 m)(− 2.5 × 10−6 m) (π) (69 × 109

N / m2 )

(4)(0.33)

= 7,800 N (1785 lbf)

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7.9 A cylindrical specimen of a hypothetical metal alloy is stressed in compression. If its original and final diameters are 30.00 and 30.04 mm, respectively, and its final length is 105.20 mm, compute its original length if the deformation is totally elastic. The elastic and shear moduli for this alloy are 65.5 and 25.4 GPa, respectively.

Solution This problem asks that we compute the original length of a cylindrical specimen that is stressed in compression. It is first convenient to compute the lateral strain εx as

εx =

Δd 30.04 mm − 30.00 mm = = 1.33 × 10-3 d0 30.00 mm

In order to determine the longitudinal strain εz we need Poisson's ratio, which may be computed using Equation 7.9; solving for ν yields

ν =

65.5 × 103 MPa E −1 = − 1 = 0.289 2G (2) (25.4 × 103 MPa )

Now εz may be computed from Equation 7.8 as ε 1.33 × 10−3 = − 4.60 × 10-3 εz = − x = − ν 0.289

Now solving for l0 using Equation 7.2

l0 =

=

li

1 + εz

105.20 mm = 105.69 mm 1 − 4.60 × 10−3

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7.10 A brass alloy is known to have a yield strength of 240 MPa (35,000 psi), a tensile strength of 310

MPa (45,000 psi), and an elastic modulus of 110 GPa (16.0 × 106 psi). A cylindrical specimen of this alloy 15.2 mm (0.60 in.) in diameter and 380 mm (15.0 in.) long is stressed in tension and found to elongate 1.9 mm (0.075 in.). On the basis of the information given, is it possible to compute the magnitude of the load that is necessary to produce this change in length? If so, calculate the load. If not, explain why.

Solution We are asked to ascertain whether or not it is possible to compute, for brass, the magnitude of the load necessary to produce an elongation of 1.9 mm (0.075 in.). It is first necessary to compute the strain at yielding from the yield strength and the elastic modulus, and then the strain experienced by the test specimen. Then, if ε(test) < ε(yield) deformation is elastic, and the load may be computed using Equations 7.1 and 7.5. However, if ε(test) > ε(yield) computation of the load is not possible inasmuch as deformation is plastic and we have neither a stress-strain plot nor a mathematical expression relating plastic stress and strain. We compute these two strain values as ε(test) =

and ε(yield) =

σy E

1.9 mm Δl = = 0.005 380 mm l0

=

240 MPa = 0.0022 110 × 103 MPa

Therefore, computation of the load is not possible since ε(test) > ε(yield).

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7.11 Consider the brass alloy for which the stress–strain behavior is shown in Figure 7.12. A cylindrical

specimen of this material 10.0 mm (0.39 in.) in diameter and 101.6 mm (4.0 in.) long is pulled in tension with a force of 10,000 N (2250 lbf). If it is known that this alloy has a value for Poisson’s ratio of 0.35, compute (a) the specimen elongation, and (b) the reduction in specimen diameter.

Solution (a) This portion of the problem asks that we compute the elongation of the brass specimen. The first calculation necessary is that of the applied stress using Equation 7.1, as

σ =

F = A0

F 2

⎛d ⎞ π⎜ 0 ⎟ ⎝2⎠

=

10,000 N ⎛ 10 × 10−3 m ⎞2 π⎜ ⎟ 2 ⎝ ⎠

= 127 MPa (17, 900 psi)

From the stress-strain plot in Figure 7.12, this stress corresponds to a strain of about 1.5 x 10-3. From the definition of strain, Equation 7.2 Δl = ε l0 = (1.5 × 10-3 ) (101.6 mm) = 0.15 mm (6.0 × 10-3 in.)

(b) In order to determine the reduction in diameter ∆d, it is necessary to use Equation 7.8 and the definition of lateral strain (i.e., εx = ∆d/d0) as follows Δd = d0εx = − d0 ν ε z = −(10 mm)(0.35) (1.5 × 10-3 )

= –5.25 × 10-3 mm (–2.05 × 10-4 in.)

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7.12 A cylindrical rod 500 mm (20.0 in.) long, having a diameter of 12.7 mm (0.50 in.), is to be subjected

to a tensile load. If the rod is to experience neither plastic deformation nor an elongation of more than 1.3 mm (0.05 in.) when the applied load is 29,000 N (6500 lbf), which of the four metals or alloys listed below are possible candidates? Justify your choice(s).

Material

Modulus of Elasticity (GPa)

Yield Strength (MPa)

Tensile Strength (MPa)

Aluminum alloy