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author | priyanka | 2015-06-24 15:03:17 +0530 |
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committer | priyanka | 2015-06-24 15:03:17 +0530 |
commit | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (patch) | |
tree | ab291cffc65280e58ac82470ba63fbcca7805165 /3257/CH2 | |
download | Scilab-TBC-Uploads-b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b.tar.gz Scilab-TBC-Uploads-b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b.tar.bz2 Scilab-TBC-Uploads-b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b.zip |
initial commit / add all books
Diffstat (limited to '3257/CH2')
-rwxr-xr-x | 3257/CH2/EX2.1/Ex2_1.sce | 14 | ||||
-rwxr-xr-x | 3257/CH2/EX2.1/Ex2_1.txt | 4 | ||||
-rwxr-xr-x | 3257/CH2/EX2.3/Ex2_3.sce | 12 | ||||
-rwxr-xr-x | 3257/CH2/EX2.3/Ex2_3.txt | 3 | ||||
-rwxr-xr-x | 3257/CH2/EX2.4/Ex2_4.sce | 14 | ||||
-rwxr-xr-x | 3257/CH2/EX2.4/Ex2_4.txt | 2 | ||||
-rwxr-xr-x | 3257/CH2/EX2.5/Ex2_5.sce | 16 | ||||
-rwxr-xr-x | 3257/CH2/EX2.5/Ex2_5.txt | 5 | ||||
-rwxr-xr-x | 3257/CH2/EX2.8/Ex2_8.sce | 18 | ||||
-rwxr-xr-x | 3257/CH2/EX2.8/Ex2_8.txt | 3 |
10 files changed, 91 insertions, 0 deletions
diff --git a/3257/CH2/EX2.1/Ex2_1.sce b/3257/CH2/EX2.1/Ex2_1.sce new file mode 100755 index 000000000..25890574d --- /dev/null +++ b/3257/CH2/EX2.1/Ex2_1.sce @@ -0,0 +1,14 @@ +// Calculation of ultimate tensile strength
+clc
+K = 689655 // in kPa
+n = 0.5
+A0 = 1 // let
+printf("\n Example 2.1")
+sigma = K*n^n
+A_neck = A0*exp(-n)
+P= sigma*A_neck
+UTS = P/A0
+printf("\n True ultimate tensile strength is %.2fkPa",sigma)
+printf("\n Engineering UTS of material is %.2f kPa",UTS)
+// Answer in book is 295521.79 kPa
+
diff --git a/3257/CH2/EX2.1/Ex2_1.txt b/3257/CH2/EX2.1/Ex2_1.txt new file mode 100755 index 000000000..2dcd1321b --- /dev/null +++ b/3257/CH2/EX2.1/Ex2_1.txt @@ -0,0 +1,4 @@ +
+ Example 2.1
+ True ultimate tensile strength is 487659.73kPa
+ Engineering UTS of material is 295780.58 kPa
\ No newline at end of file diff --git a/3257/CH2/EX2.3/Ex2_3.sce b/3257/CH2/EX2.3/Ex2_3.sce new file mode 100755 index 000000000..48b9448f9 --- /dev/null +++ b/3257/CH2/EX2.3/Ex2_3.sce @@ -0,0 +1,12 @@ +// Calculation of modulus resilience from hardness
+clc
+h = 400 // hardness of specimen in HB
+E = 205e3 // Youngs modulus of steel in MPa
+g = 9.8 // gravitational acceleration in m/s^2
+printf("\n Example 2.3")
+Y = h*1e6*g/3 // As, Hardness = c*Y
+m_r = (Y/1e6)^2/(2*E) // modulus of resilience
+
+printf("\n Modulus of resilience of body is %.2f Nm/m^3.", m_r)
+// while numerical value of answer in book is 4.17
+
diff --git a/3257/CH2/EX2.3/Ex2_3.txt b/3257/CH2/EX2.3/Ex2_3.txt new file mode 100755 index 000000000..0277c593e --- /dev/null +++ b/3257/CH2/EX2.3/Ex2_3.txt @@ -0,0 +1,3 @@ +
+ Example 2.3
+ Modulus of resilience of body is 4.16 Nm/m^3.
\ No newline at end of file diff --git a/3257/CH2/EX2.4/Ex2_4.sce b/3257/CH2/EX2.4/Ex2_4.sce new file mode 100755 index 000000000..a067740d1 --- /dev/null +++ b/3257/CH2/EX2.4/Ex2_4.sce @@ -0,0 +1,14 @@ +// Elimination of stress by tension
+clc
+sigma_t = 140 // in MPa
+sigma_c = -140 // in MPa
+l = 0.25 // length of specimen in m
+Y = 150 // yield stress of material in MPa
+E = 70 // Youngs modulus in GPa
+printf("\ Example 2.4")
+epsilon_tot = (sigma_c*1e6)/(E*1e9) + Y*1e6/(E*1e9) // total strain
+l_f = l*exp(epsilon_tot)
+
+printf("\n Stretched length should be %0.4f m",l_f)
+// Numerical value of answer in book is 0.2510
+
diff --git a/3257/CH2/EX2.4/Ex2_4.txt b/3257/CH2/EX2.4/Ex2_4.txt new file mode 100755 index 000000000..f3fa125a6 --- /dev/null +++ b/3257/CH2/EX2.4/Ex2_4.txt @@ -0,0 +1,2 @@ + Example 2.4
+ Stretched length should be 0.2500 m
\ No newline at end of file diff --git a/3257/CH2/EX2.5/Ex2_5.sce b/3257/CH2/EX2.5/Ex2_5.sce new file mode 100755 index 000000000..91dfe23c0 --- /dev/null +++ b/3257/CH2/EX2.5/Ex2_5.sce @@ -0,0 +1,16 @@ +// Yielding of a thin walled shell
+clc
+r = 254 // radius in mm
+t = 2.54 // thickness in mm
+sigma_1 = 140 // stress in MPa
+sigma_2 = 140 // stress in MPa
+sigma_min = 0 // stress in MPa
+printf("\ Example 2.5")
+Y = sigma_2 - sigma_min
+p = 2*(t/1e3)*Y/(r*1e-3)
+printf("\n\n According to maximum shear stress criterion, Required pressure is %.1f MPa",p)
+Y = sqrt(0.5*(sigma_1^2+sigma_2^2))
+p = 2*(t/1e3)*Y/(r*1e-3)
+printf("\n\n According to maximum distortion energy criterion, Required pressure is %.1f MPa",p)
+
+
diff --git a/3257/CH2/EX2.5/Ex2_5.txt b/3257/CH2/EX2.5/Ex2_5.txt new file mode 100755 index 000000000..9c8488de6 --- /dev/null +++ b/3257/CH2/EX2.5/Ex2_5.txt @@ -0,0 +1,5 @@ + Example 2.5
+
+ According to maximum shear stress criterion, Required pressure is 2.8 MPa.
+
+ According to maximum distortion energy criterion, Required pressure is 2.8 MPa.
\ No newline at end of file diff --git a/3257/CH2/EX2.8/Ex2_8.sce b/3257/CH2/EX2.8/Ex2_8.sce new file mode 100755 index 000000000..e6b30d838 --- /dev/null +++ b/3257/CH2/EX2.8/Ex2_8.sce @@ -0,0 +1,18 @@ +// Temperature rise in simple deformation
+clc
+d = 25 // diameter of cylinder in mm
+h_i = 25 // Height of cylinder in mm
+cp = 1255 // specific heat capacity in J/kg.K
+rho = 2768 // density in kg
+del_t = 55 // temperature change in K
+K = 104 // in MPa
+n = 0.5
+printf("\n Example 2.8")
+v = %pi/4*(d*1e-3)^2*h_i*1e-3 // volume of cylinder
+H = cp*rho*v*del_t // heat in Joule
+
+epsilon = (H/(v*K*1e6/(n+1)))^(1/(n+1))
+h_f = h_i/exp(epsilon)
+
+printf("\n Final height of specimen is %.1f mm",h_f)
+
diff --git a/3257/CH2/EX2.8/Ex2_8.txt b/3257/CH2/EX2.8/Ex2_8.txt new file mode 100755 index 000000000..4a6331e4d --- /dev/null +++ b/3257/CH2/EX2.8/Ex2_8.txt @@ -0,0 +1,3 @@ +
+ Example 2.8
+ Final height of specimen is 3.5 mm.
\ No newline at end of file |