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+//find
+clc
+//solution
+//given
+P=15000//W
+q=(%pi/180)*20
+a=(%pi/180)*45
+Np=10000//rpm
+Dp=0.08//m
+Dg=0.32//m
+fop=100
+fog=100
+fes=618
+//let m is module
+T=P*60/(2*%pi*Np)//N-m
+Wt=T/(Dp/2)//N
+//Tp=Dp/m
+//Te=Tp/(cos(a))^3=226.4/m
+//ypb=0.175-(0.841/Te)=0.175-0.0037m
+v=%pi*Dp*Np/60//m/s
+Cv=0.75/(0.75+sqrt(v))
+//b=12.5m...assume
+//Wt=fop*Cv*b*%pi*m*ypb=72m^2-1.5m^3
+//using hit and trial m=2.3..say 2.5
+m=2.5
+b=12.5*m
+printf("module and face width is,%f mm\n,%f mm\n",m,b)
+vr=Dg/Dp
+Q=2*vr/(vr+1)
+//x=tan(qn)
+x=tan(q)*tan(a)
+qn=(%pi/180)*14.4
+Ep=200*1000
+Eg=200*1000
+K=(fes)^2*sin(qn)*(1/1.4)*(1/Ep +1/Eg)//N/mm^2
+Ww=Dp*b*Q*K*1000/(cos(a))^2//N
+printf("load stress factor is,%f N/mm^2\n",K)
+printf("wear load acting is,%f N\n",Ww)
+printf("since wear load acting is more then tangentia tooth load ,hence design is safe") \ No newline at end of file