1 files changed, 20 insertions, 20 deletions
diff --git a/278/CH10/EX10.10/ex_10_10.sce b/278/CH10/EX10.10/ex_10_10.sce
index 505bc826a..ac247d7fd 100755
--- a/278/CH10/EX10.10/ex_10_10.sce
+++ b/278/CH10/EX10.10/ex_10_10.sce
@@ -1,20 +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)
+
+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)