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Unit Cells Metallic Crystal Structures 3.2 If the atomic radius of lead is 0.175 nm, calculate the volume of its unit cell in cubic meters. Solution Lead has an FCC crystal structure and an atomic radius of 0.1750 nm (Table 3.1). The FCC unit cell volume may be computed from Equation 3.6 as 3.3 Show for the body-centered cubic crystal structure that the unit cell edge length a and the atomic radius R are related through . Solution This problem calls for a demonstration of the relationship for BCC. Consider the BCC unit cell shown below From the triangle NOP And then for triangle NPQ, But = 4R, R being the atomic radius. Also, = a. Therefore, And solving for a: 3.4 For the HCP crystal structure, show that the ideal c/a ratio is 1.633. Solution We are asked to show that the ideal c/a ratio for HCP is 1.633. A sketch of one-third of an HCP unit cell is shown below. Consider the tetrahedron labeled as JKLM, which is reconstructed as follows: The atom at point M is midway between the top and bottom faces of the unit cell--that is = c/2. And, since atoms at points J, K, and M, all touch one another, where R is the atomic radius. Furthermore, from triangle JHM, or Now, we can determine the length by consideration of triangle JKL, which is an equilateral triangle, From this triangle it is the case that the angle subtended between the lines and is 30°, and which reduces to the following: Substitution of this value for into the above expression yields And when we solve for c/a 3.5 Show that the atomic packing factor for BCC is 0.68. Solution The atomic packing factor is defined as the ratio of sphere volume (VS ) to the total unit cell volume (VC ), or Because there are two spheres associated with each unit cell for BCC Also, the unit cell has cubic symmetry, that is VC = a3. But a depends on R according to Equation 3.4, and Thus, 3.6 Show that the atomic packing factor for HCP is 0.74. Solution The APF is just the total sphere volume-unit cell volume ratio—i.e., (VS /VC ) . For HCP, there are the equivalent of six spheres per unit cell, and thus The unit cell volume (VC) for the HCP unit cell was determined in Example Problem 3.3 and given in Equation 3.7b as And because c = 1.633a = 2R(1.633) Thus, Density Computations 3.7 Molybdenum (Mo) has a BCC crystal structure, an atomic radius of 0.1363 nm, and an atomic weight of 95.94 g/mol. Compute and compare its theoretical density with the experimental value found inside the front cover of the book. Solution This problem calls for a computation of the density of molybdenum. According to Equation 3.8 For BCC, n = 2 atoms/unit cell. Furthermore, because VC = a3, and (Equation 3.4), then Thus, realizing that AMo = 95.94 g/mol, using the above version of Equation 3.8, we compute the theoretical density for Mo as follows: = 10.22 g/cm3 The value given inside the front cover is 10.22 g/cm3. 3.8 Strontium (Sr) has an FCC crystal structure, an atomic radius of 0.215 nm and an atomic weight of 87.62 g/mol. Calculate the theoretical density for Sr. Solution According to Equation 3.8 For FCC, n = 4 atoms/unit cell. Furthermore, because VC = a3, and (Equation 3.1), then Thus, realizing that ASr = 87.62 g/mol, using the above version of Equation 3.8, we compute the theoretical density of Sr as follows: = 2.59 g/cm3 The experimental density for Sr is 2.54 g/cm3. 3.9 Calculate the radius of a palladium (Pd) atom, given that Pd has an FCC crystal structure, a density of 12.0 g/cm3, and an atomic weight of 106.4 g/mol. Solution We are asked to determine the radius of a palladium atom, given that Pd has an FCC crystal structure. For FCC, n = 4 atoms/unit cell, and (Equation 3.6). Now, the density of Pd may be expressed using a form of Equation 3.8 as follows: Solving for R from the above expression yields Incorporation into this expression values for APd , n, and ρ leads to the following value of R: = 1.38 × 10-8 cm = 0.138 nm 3.10 Calculate the radius of a tantalum (Ta) atom, given that Ta has a BCC crystal structure, a density of 16.6 g/cm3, and an atomic weight of 180.9 g/mol. Solution It is possible to compute the radius of a Ta atom using a rearranged form of Equation 3.8. For BCC, n = 2 atoms/unit cell. Furthermore, because VC = a3 and (Equation 3.4) an expression for the BCC unit cell volume is as follows: For Ta, Equation 3.8 takes the form Solving for R in this equation yields Upon incorporation of values of n, ATa, and ρ into this equation leads to the atomic radius of Ta as follows: = 1.43 × 10−8 cm = 0.143 nm ch02 ch03 ch04 ch05 ch06 ch07 ch08 ch09 ch10 CHAPTER 10 PHASE TRANSFORMATIONS PROBLEM SOLUTIONS Differentiation of this expression with respect to a is as If we set this expression equal to zero as Substitution of this expression for a in the above expression for G yields an equation for G* as For computation of the activation free energy, Equation 10.7 is employed. Thus Inasmuch as 4 atoms are associated with each FCC unit cell, the total number of atoms per critical nucleus is just Now for 200 K supercooling, it is first necessary to recalculate the value G* of using Equation 10.7, where, again, the T42Tm42T – T term is replaced by the number of degrees of supercooling, denoted as T, which in this case is 200 K. Thus And, from Equation 10.8, the value of n* is Now, for 300 K supercooling the value of G* is equal to We now want to manipulate Equation 10.17 such that t is the dependent variable. The above Equation 10.17a may be written in the form: And solving this expression for t leads to Now, using this equation and the value of k determined above, the time to 90% transformation completion is equal to Now, solving for t from this expression leads to Now, the rate is computed using Equation 10.18 as At this point we want to compute t41T0.541T, the value of t for y = 0.5, which means that it is necessary to establish a form of Equation 10.17 in which t is the dependent variable. Rearrangement of Equation 10.17b above leads to And solving this expression for t leads to And solving for t leads to ch11 ch12 ch12_A ch12_B ch13 ch14 ch15 ch16 Using a modified form of Equation 16.2, the minimum thermal conductivity k40Tmin40T is And for the specific gravity Therefore, we compute the specific stiffness as follows: Or, when x = 1.25 mm (0.05 in.) and = 0.90, then (a) The longitudinal tensile strength is determined using Equation 16.17 as follows: (b) The longitudinal elastic modulus is computed using Equation 16.10a as While transverse modulus expression is as follows: Solving these two expressions simultaneously for E41Tm41T and E41Tf41T leads to the following values: For elastic deformation, combining Equations 6.1 and 6.5 yields the following expression: But, we may write the following expression as a way of defining Vm: Vm = Am/Ac which, upon rearrangement gives Now, the volume fraction of fibers is equal to Vm = Am/Ac; upon substitution of this expression for V40Tm40T into Equation S16.11f leads to the following: Now, using values for F41Tf41T and F41Tm41T from the problem statement And substitution of the values for E41Tf41T and E41Tm41T given in the problem statement into the first equation above leads to And, solving for V41Tf41T yields, V41Tf41T = 0.258. (b) We are now asked for the tensile strength of this composite. The computation requires the use of Equation 16.17—viz., Which means that F41Tf41T= 44.7F41Tm41T. Now, the stresses of each of the fiber and matrix phases are determined using Equation 6.1 as follows: Or, solving for V40Tf Also And, an expression for 41Tm41T analogous to the one for 41Tf41T given in Equation S16.14a above is as follows: From which we solve for F41Tm41T as follows: Inasmuch as l >> l41Tc41T (that is, 8.0 mm >> 0.18 mm), then use of Equation 16.17 is appropriate. Therefore, Inasmuch as l < lc (0.50 mm < 0.80 mm), then use of Equation 16.19 is required. Therefore, Solving this expression for V41Tf41T leads to V41Tf41T = 0.397. Solving this expression for K yields For Vf = 0.3 And, for Vf = 0.4 For the carbon-fiber reinforced epoxy And, for the aramid-fiber reinforced epoxy For the normalized 1040 plain carbon steel, the ratio is For the 7075-T6 aluminum alloy For the C26000 brass (cold worked) For the AZ31B (extruded) magnesium alloy For the annealed Ti-5Al-2.5Sn titanium alloy For the carbon-fiber reinforced epoxy And, for the aramid-fiber reinforced epoxy For the normalized 1040 plain-carbon steel For the 7075-T6 aluminum alloy For the cold worked C26000 brass For the extruded AZ31B magnesium alloy For the Ti-5Al-2.5Sn titanium alloy And Since, in general, = /E (Equation 6.5), making substitutions of the form of Equation 6.5 into the previous expression yields the following: And, finally, taking the reciprocal of this equation leads to Because this value is less than the specified minimum (i.e., 55 GPa), glass is not an acceptable candidate. ch17 ch18 ch19 ch20 ch21