# 6.4 A cylindrical specimen of a titanium alloy having an elastic modulus of 107 GPa ( psi) and

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1 6.4 A cylindrical specimen of a titanium alloy having an elastic modulus of 107 GPa ( psi) and an original diameter of 3.8 mm (0.15 in.) will experience only elastic deformation when a tensile load of 2000 N (450 lb f ) is applied. Compute the maximum length of the specimen before deformation if the maximum allowable elongation is 0.42 mm ( in.). We are asked to compute the maximum length of a cylindrical titanium alloy specimen (before deformation) that is deformed elastically in tension. or a cylindrical specimen A 0 π d where d 0 is the original diameter. Combining Equations 6.1, 6.2, and 6.5 and solving for l 0 leads to l 0 l ε l Ź σ E l E Ź A 0 d l Eπ l Eπ d ( m)( N / m 2 ) (π)( m) 2 (4)(2000 N) m 255 mm (10.0 in.)

2 6.8 A cylindrical rod of copper (E 110 GPa, psi) having a yield strength of 240 MPa (35,000 psi) is to be subjected to a load of 6660 N (1500 lb f ). If the length of the rod is 380 mm (15.0 in.), what must be the diameter to allow an elongation of 0.50 mm (0.020 in.)? This problem asks us to compute the diameter of a cylindrical specimen of copper in order to allow an elongation of 0.50 mm. Employing Equations 6.1, 6.2, and 6.5, assuming that deformation is entirely elastic σ A 0 π d E l l 0 Or, solving for d 0 d 0 4 l 0 π E l (4)( m) (6660 N) (π)( N / m 2 )( m) m 7.65 mm (0.30 in.)

3 6.19 Consider a cylindrical specimen of some hypothetical metal alloy that has a diameter of 8.0 mm (0.31 in.). A tensile force of 1000 N (225 lb f ) produces an elastic reduction in diameter of mm ( in.). Compute the modulus of elasticity for this alloy, given that Poisson's ratio is This problem asks that we calculate the modulus of elasticity of a metal that is stressed in tension. Combining Equations 6.5 and 6.1 leads to E σ ε z A 0 ε z ε z π d ε z π d rom the definition of Poisson's ratio, (Equation 6.8) and realizing that for the transverse strain, ε x d d 0 ε z ε x ν d d 0 ν Therefore, substitution of this expression for ε z into the above equation yields E 4 ε z π d2 4 ν π d 0 0 d (4)(1000 N)(0.30) π( m)( m) Pa GPa ( psi)

4 6.28 A bar of a steel alloy that exhibits the stress-strain behavior shown in igure 6.21 is subjected to a tensile load; the specimen is 300 mm (12 in.) long, and of square cross section 4.5 mm (0.175 in.) on a side. (a) Compute the magnitude of the load necessary to produce an elongation of 0.45 mm (0.018 in.). (b) What will be the deformation after the load has been released? (a) We are asked to compute the magnitude of the load necessary to produce an elongation of 0.45 mm for the steel displaying the stress-strain behavior shown in igure irst, calculate the strain, and then the corresponding stress from the plot. ε l l mm 300 mm This is near the end of the elastic region; from the inset of igure 6.21, this corresponds to a stress of about 300 MPa (43,500 psi). Now, from Equation 6.1 σa 0 σb 2 in which b is the cross-section side length. Thus, ( N/m 2 )( m) N (1366 lb f ) (b) After the load is released there will be no deformation since the material was strained only elastically.

5 6.50 A steel alloy specimen having a rectangular cross section of dimensions 12.7 mm 6.4 mm (0.5 in in.) has the stress strain behavior shown in igure If this specimen is subjected to a tensile force of 38,000 N (8540 lb f ) then (a) Determine the elastic and plastic strain values. (b) If its original length is 460 mm (18.0 in.), what will be its final length after the load in part (a) is applied and then released? (a) We are asked to determine both the elastic and plastic strain values when a tensile force of 38,000 N (8540 lb f ) is applied to the steel specimen and then released. irst it becomes necessary to determine the applied stress using Equation 6.1; thus σ A 0 b 0 d 0 where b 0 and d 0 are cross-sectional width and depth (12.7 mm and 6.4 mm, respectively). Thus σ 38, 000 N ( m)( m) N / m MPa (68,300 psi) rom igure 6.21, this point is in the plastic region so the specimen will be both elastic and plastic strains. The total strain at this point, ε t, is about We are able to estimate the amount of permanent strain recovery ε e from Hooke's law, Equation 6.5 as ε e σ E And, since E 207 GPa for steel (Table 6.1) ε e 468 MPa MPa The value of the plastic strain, ε p is just the difference between the total and elastic strains; that is ε p ε t ε e

6 (b) If the initial length is 460 mm (18.0 in.) then the final specimen length l i may be determined from a rearranged form of Equation 6.2 using the plastic strain value as l i l 0 (1 + ε p ) (460 mm)( ) mm (18.14 in.)

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