1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
|
{
"metadata": {
"name": "CH7"
},
"nbformat": 3,
"nbformat_minor": 0,
"worksheets": [
{
"cells": [
{
"cell_type": "heading",
"level": 1,
"metadata": {},
"source": [
"Chapter 7: Dislocation and Strengthening Mechanisms"
]
},
{
"cell_type": "heading",
"level": 3,
"metadata": {},
"source": [
"Example 7.1 Page no 183"
]
},
{
"cell_type": "code",
"collapsed": false,
"input": [
"#Resolved Shear Stress Computations\n",
"\n",
"#Direction for given plane\n",
"u1=1\n",
"v1=1\n",
"w1=0\n",
"u2=0\n",
"v2=1\n",
"w2=0\n",
"#For lamda\n",
"u3=-1\n",
"v3=1\n",
"w3=1\n",
"\n",
"#Calculation\n",
"import math\n",
"phi=math.acos((u1*u2+v1*v2+w1*w2)/(math.sqrt((u1**2+v1**2+w1**2)*(u2**2+v2**2+w2**2))))\n",
"lam=math.acos((u3*u2+v3*v2+w3*w2)/(math.sqrt((u3**2+v3**2+w3**2)*(u2**2+v2**2+w2**2))))\n",
"sigma=52 #in MPa, Tensile stress\n",
"tr=sigma*math.cos(phi)*math.cos(lam)\n",
"trc=30 #in MPa Critical resolved shear stress\n",
"sy=trc/(math.cos(phi)*math.cos(lam))\n",
"\n",
"#Result\n",
"print\"(a)The resolved shear stress is \",round(tr,2),\"MPa\"\n",
"print\"(b)Yield strength is\",round(sy,1),\"MPa\"\n",
"\n"
],
"language": "python",
"metadata": {},
"outputs": [
{
"output_type": "stream",
"stream": "stdout",
"text": [
"(a)The resolved shear stress is 21.23 MPa\n",
"(b)Yield strength is 73.5 MPa\n"
]
}
],
"prompt_number": 19
},
{
"cell_type": "heading",
"level": 3,
"metadata": {},
"source": [
"Example 7.2 Page no 194"
]
},
{
"cell_type": "code",
"collapsed": false,
"input": [
"#Tensile Strength and Ductility Determinations for Cold-Worked Copper\n",
"\n",
"#Given\n",
"df=12.2 #Final dia in mm\n",
"di=15.2 #Initial dia in mm\n",
"\n",
"#Calculation\n",
"CW = ((di**2-df**2)/di**2)*100\n",
"ts=340 #in Mpa tensile strength, from fig 7.19 (b)\n",
"duc=7 #in % Ductility from fig 7.19 (c)\n",
"\n",
"#result\n",
"print\"Percent Cold Work is \",round(CW,1),\"%\"\n",
"print\"Tensile strength is\",ts,\"MPa\"\n",
"print\"Ductility is \",duc,\"%\"\n",
"\n"
],
"language": "python",
"metadata": {},
"outputs": [
{
"output_type": "stream",
"stream": "stdout",
"text": [
"Percent Cold Work is 35.6 %\n",
"Tensile strength is 340 MPa\n",
"Ductility is 7 %\n"
]
}
],
"prompt_number": 6
},
{
"cell_type": "heading",
"level": 3,
"metadata": {},
"source": [
"Design Example 7.3 Page no 199"
]
},
{
"cell_type": "code",
"collapsed": false,
"input": [
"#Description of Diameter Reduction Procedure\n",
"\n",
"#Given\n",
"di=6.4 #Initial dia in mm\n",
"df=5.1 #Final dia in mm\n",
"\n",
"#Calculation\n",
"#Cold Work Computation\n",
"CW = ((di**2-df**2)/di**2)*100\n",
"#From Figures 7.19a and 7.19c, \n",
"#A yield strength of 410 MPa \n",
"#And a ductility of 8% EL are attained from this deformation\n",
"dmid = math.sqrt(df**2/(1-0.215))\n",
"\n",
"#Result\n",
"print\"Cold work is \",round(CW,1),\"%\"\n",
"print\"But required ductility and yield strength is not matched at this cold work\"\n",
"print\"Hence required Cold work is 21.5 %\"\n",
"print\"Hence original diameter for second drawing is \",round(dmid,1),\"mm\"\n",
"\n"
],
"language": "python",
"metadata": {},
"outputs": [
{
"output_type": "stream",
"stream": "stdout",
"text": [
"Cold work is 36.5 %\n",
"But required ductility and yield strength is not matched at this cold work\n",
"Hence required Cold work is 21.5 %\n",
"Hence original diameter for second drawing is 5.8 mm\n"
]
}
],
"prompt_number": 11
},
{
"cell_type": "code",
"collapsed": false,
"input": [],
"language": "python",
"metadata": {},
"outputs": []
}
],
"metadata": {}
}
]
}
|