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author | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
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committer | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
commit | 7f60ea012dd2524dae921a2a35adbf7ef21f2bb6 (patch) | |
tree | dbb9e3ddb5fc829e7c5c7e6be99b2c4ba356132c /3647/CH9 | |
parent | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (diff) | |
download | Scilab-TBC-Uploads-7f60ea012dd2524dae921a2a35adbf7ef21f2bb6.tar.gz Scilab-TBC-Uploads-7f60ea012dd2524dae921a2a35adbf7ef21f2bb6.tar.bz2 Scilab-TBC-Uploads-7f60ea012dd2524dae921a2a35adbf7ef21f2bb6.zip |
initial commit / add all books
Diffstat (limited to '3647/CH9')
-rw-r--r-- | 3647/CH9/EX9.1/ex9_1.sce | 14 | ||||
-rw-r--r-- | 3647/CH9/EX9.2/ex9_2.sce | 12 | ||||
-rw-r--r-- | 3647/CH9/EX9.3/ex9_3.sce | 21 | ||||
-rw-r--r-- | 3647/CH9/EX9.4/ex9_4.sce | 26 | ||||
-rw-r--r-- | 3647/CH9/EX9.5/ex9_5.sce | 20 | ||||
-rw-r--r-- | 3647/CH9/EX9.6/Ex9_6.sce | 24 |
6 files changed, 117 insertions, 0 deletions
diff --git a/3647/CH9/EX9.1/ex9_1.sce b/3647/CH9/EX9.1/ex9_1.sce new file mode 100644 index 000000000..7b196d720 --- /dev/null +++ b/3647/CH9/EX9.1/ex9_1.sce @@ -0,0 +1,14 @@ +//Solutions to Problems In applied mechanics +//A N Gobby +clear all; +clc
+//initialisation of variables
+q=8000//lbf/in^2
+r=9.25//in
+G=12*10^6//lbf/in^2
+t=1*%pi/180//rad
+h=180//lbf ft
+//CALCULATIONS
+S=((G*%pi*r)/(q*h*2))//in
+//RESULTS
+printf('the shaft size and maximum shear stress=% f in',S)
diff --git a/3647/CH9/EX9.2/ex9_2.sce b/3647/CH9/EX9.2/ex9_2.sce new file mode 100644 index 000000000..18ba7f359 --- /dev/null +++ b/3647/CH9/EX9.2/ex9_2.sce @@ -0,0 +1,12 @@ +//Solutions to Problems In applied mechanics +//A N Gobby +clear all; +clc
+//initialisation of variables
+a=600000//lbf in
+b=%pi*(4)^4/32//in^2
+q=4000//in^2
+//CALCULATIONS
+D=sqrt((a)/q)*2/b*10//in
+//RESULTS
+printf('The shaft diameter=% f in',D)
diff --git a/3647/CH9/EX9.3/ex9_3.sce b/3647/CH9/EX9.3/ex9_3.sce new file mode 100644 index 000000000..c7a8ac20c --- /dev/null +++ b/3647/CH9/EX9.3/ex9_3.sce @@ -0,0 +1,21 @@ +//Solutions to Problems In applied mechanics +//A N Gobby +clear all; +clc
+//initialisation of variables
+h1=4//in
+d=40//hp
+w=30//rev/min
+t=33*1/3//degree
+h=33000//lbf ft
+G=12*10^6//lbf/in^2
+q=1.33//lbf ft
+j=12//in
+//CALCULATIONS
+M=((h*d)/(2*%pi*w))//lbf ft
+N=M*q//lbf ft
+H=((N*j*h1*1/2)/(%pi*(h1)^4/32))//lbf/in^2
+A=((j*N*j*180)/(%pi*(h1)^4/32*G*%pi))//degree
+//RESULTS
+printf('the maximum shear stress=% f lbf/in^2',H)
+printf('the angle of twist=% f degree',A)
diff --git a/3647/CH9/EX9.4/ex9_4.sce b/3647/CH9/EX9.4/ex9_4.sce new file mode 100644 index 000000000..b0d1ab757 --- /dev/null +++ b/3647/CH9/EX9.4/ex9_4.sce @@ -0,0 +1,26 @@ +//Solutions to Problems In applied mechanics +//A N Gobby +clear all; +clc
+//initialisation of variables
+h=6//in
+h1=4//in
+d=5000//kilowatt
+g=2500//rev/min
+f=8//in
+l=20//in
+G=12*10^6//lbf/in^2
+p=746//watts
+w=1000//in
+q=33000//in
+j=102.2//in^4
+t=12//in
+k=180//in
+//CALCULATIONS
+S=(d*w/p)//hp
+T=((q*S)/(2*%pi*g))//lbf ft
+Q=(t*T/j)*3//lbf/in^2
+F=f*Q//lbf/in^2
+A=((t*T*l*h*k)/(G*j*%pi))//degree
+//RESULTS
+printf('the angle of twist=% f degree',A)
diff --git a/3647/CH9/EX9.5/ex9_5.sce b/3647/CH9/EX9.5/ex9_5.sce new file mode 100644 index 000000000..3ab32b3be --- /dev/null +++ b/3647/CH9/EX9.5/ex9_5.sce @@ -0,0 +1,20 @@ +//Solutions to Problems In applied mechanics +//A N Gobby +clear all; +clc
+//initialisation of variables
+d=7.5//in
+m1=8000//lbf/in^2
+m2=2000//lbf/in^2
+h1=3//in
+d1=2//in
+d4=57//lbf in
+W=2.74//lbf in
+//CALCULATIONS
+P=%pi*d1^4/32//in^4
+M=(m1/1)*P//lbf in
+T=M/(8*(d/d1))//lbf
+A=T/m2//in^2
+B=sqrt((4*A)/%pi)//in
+//RESULTS
+printf('the bolt diameter =% f in',B)
diff --git a/3647/CH9/EX9.6/Ex9_6.sce b/3647/CH9/EX9.6/Ex9_6.sce new file mode 100644 index 000000000..0f0ab5ec5 --- /dev/null +++ b/3647/CH9/EX9.6/Ex9_6.sce @@ -0,0 +1,24 @@ +//Solutions to Problems In applied mechanics +//A N Gobby +clear; + +clc +//initialisation of variables +d=30//in +w=50//lbf ft +d1=10//in +G=12*10^6//lbf/in^2 +T1=50//lbf ft +T2=16.7//lbf ft +J=4810//lbf ft +TA=w/3//lbf ft +Tab=w-TA//lbf ft +//CALCULATIONS +Ta=Tab-TA//lbf ft +T3=Tab-TA //lbf ft +Qmax=T3*G*(3/8)/(%pi/32)*(3/4)^4//lbf/in^2 +M=(T3*12*d1)/(%pi/4*(3/4)^4*G)*(180/%pi)//degree +//RESULTS +printf('The couples required to hold the ends=% f lbf ft',Ta) +printf('The magnitude of the greatest shear stress set up in the shaft=% f lbf/in^2',Qmax) +printf('the angular rotation in degree of the section=% f degree',M)
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