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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 /278/CH10/EX10.10 | |
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initial commit / add all books
Diffstat (limited to '278/CH10/EX10.10')
-rwxr-xr-x | 278/CH10/EX10.10/ex_10_10.sce | 20 |
1 files changed, 20 insertions, 0 deletions
diff --git a/278/CH10/EX10.10/ex_10_10.sce b/278/CH10/EX10.10/ex_10_10.sce new file mode 100755 index 000000000..505bc826a --- /dev/null +++ b/278/CH10/EX10.10/ex_10_10.sce @@ -0,0 +1,20 @@ +//find max noraml and shear stress
+clc
+//solution
+//given
+//ref fig 10.25
+D=50//mm
+s=15//mm
+P=10000//N
+e=200//mm
+//let t is thickness of throat
+//A=t*pi*D
+pi=3.14
+A=0.707*s*pi*D//mm^2
+t=P/A//N/mm^2
+M=P*e//N-mm
+Z=pi*.707*s*D^2/4//mm^3
+fb=M/Z//N/mm^2
+ftmax=(0.5*fb)+(0.5*sqrt(fb^2+4*t^2))//N/mm^2
+Tmax=(0.5*sqrt(fb^2+4*t^2))//N/mm^2
+printf("the max normal stress and shear stress are,%f N/mm^2\n,%f N/mm^2 respectively",ftmax,Tmax)
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