2 files changed, 39 insertions, 38 deletions
diff --git a/866/CH14/EX14.1/14_1.sce b/866/CH14/EX14.1/14_1.sce
index 7ead5d32e..d92386d33 100755
--- a/866/CH14/EX14.1/14_1.sce
+++ b/866/CH14/EX14.1/14_1.sce
@@ -1,19 +1,20 @@
-clc
-//initialisation of variables
-d= 2 //m
-t= 20 //mm
-p= 1.5 //N/mm^2
-load= 2500 //KN
-alpha= 60 //degrees
-//CALCULATIONS
-Cs= (p*d*10^3)/(2*t)
-Ls= (p*d*10^3)/(4*t)
-Ds= (load*10^3)/(%pi*d*t*10^3)
-Ts= Ls+Ds
-sigman= (Ts*t*(cosd(90-alpha))^2+Cs*t*(cosd(alpha))^2)/t
-tab= Ts*sind(alpha)*cosd(alpha)-Cs*sind(alpha)*cosd(alpha)
-tmax= (Ts-Cs)/2
-//RESULTS
-printf ('direct stress= %.1f N/mm^2',sigman)
-printf (' \n Shear stress=%.1f N/mm^2',tab)
-printf (' \n maximum Shear stress=%.1f N/mm^2',tmax)
+clc
+clear
+//initialisation of variables
+d= 2 //m
+t= 20 //mm
+p= 1.5 //N/mm^2
+Load= 2500 //KN
+alpha= 60 //degrees
+//CALCULATIONS
+Cs= (p*d*10^3)/(2*t)
+Ls= (p*d*10^3)/(4*t)
+Ds= (Load*10^3)/(%pi*d*t*10^3)
+Ts= Ls+Ds
+sigman= (Ts*t*(cosd(90-alpha))^2+Cs*t*(cosd(alpha))^2)/t
+tab= Ts*sind(alpha)*cosd(alpha)-Cs*sind(alpha)*cosd(alpha)
+tmax= (Ts-Cs)/2
+//RESULTS
+printf ('direct stress= %.1f N/mm^2',sigman)
+printf (' \n Shear stress=%.1f N/mm^2',tab)
+printf (' \n maximum Shear stress=%.1f N/mm^2',tmax)
+\ No newline at end of file
diff --git a/866/CH14/EX14.2/14_2.sce b/866/CH14/EX14.2/14_2.sce
index 12ff51aff..d32f2d3e2 100755
--- a/866/CH14/EX14.2/14_2.sce
+++ b/866/CH14/EX14.2/14_2.sce
@@ -1,19 +1,19 @@
-clc
-//initialisation of variables
-load= 50000 //N
-torque= 1200 //Nm
-d= 60//mm
-t= 1.5 //mm
-alpha= 60 //degrees 
-//CALCULATIONS
-BM= load*t
-axialload= (load*4)/(%pi*d^2)
-bendingmoment= (BM*d*64)/(%pi*d^4*2)
-Ts= axialload+bendingmoment
-shearstress= (torque*10^3*d*32)/(2*%pi*d^4)
-sigman= -Ts*(cosd(alpha-30))^2+shearstress*cosd(alpha-30)*sind(alpha-30)+shearstress*cosd(alpha-30)*sind(alpha-30)
-T= -Ts*sind(alpha)*cosd(alpha)-shearstress*(sind(alpha))^2+shearstress*(cosd(alpha)^2)
-//RESULTS
-printf ('direct stress= %.1f N/mm^2',sigman)
-printf (' \n Shear stress=%.1f N/mm^2',T)
-
+clc
+clear
+//initialisation of variables
+Load= 50000 //N
+torque= 1200 //Nm
+d= 60//mm
+t= 1.5 //mm
+alpha= 60 //degrees 
+//CALCULATIONS
+BM= Load*t
+axialLoad= (Load*4)/(%pi*d^2)
+bendingmoment= (BM*d*64)/(%pi*d^4*2)
+Ts= axialLoad+bendingmoment
+shearstress= (torque*10^3*d*32)/(2*%pi*d^4)
+sigman= -Ts*(cosd(alpha-30))^2+shearstress*cosd(alpha-30)*sind(alpha-30)+shearstress*cosd(alpha-30)*sind(alpha-30)
+T= -Ts*sind(alpha)*cosd(alpha)-shearstress*(sind(alpha))^2+shearstress*(cosd(alpha)^2)
+//RESULTS
+printf ('direct stress= %.1f N/mm^2',sigman)
+printf (' \n Shear stress=%.1f N/mm^2',T)
+\ No newline at end of file