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authorprashantsinalkar2017-10-10 12:27:19 +0530
committerprashantsinalkar2017-10-10 12:27:19 +0530
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+Bf=1250//width of flange, in mm
+Df=120//thickness of flange, in mm
+d=700//effective depth, in mm
+m=13.33//modular ratio
+Ast=5500//in sq mm
+W=60//UDL including self-weight, in kN/m
+l=8//span, in m
+M=W*l^2/8*10^6//in N-mm
+//Assume x>Df. Equating moments of area on compressiona and tension sides about N.A.
+x=(m*Ast*d+Bf*Df^2/2)/(m*Ast+Bf*Df)//in mm
+//let sigma_cbc_dash=a*sigma_cbc
+a=(x-Df)/x
+//to find lever arm
+z=d-(1+2*a)/(1+a)*Df/3//in mm
+sigma_cbc=2*M/(Bf*Df*(1+a)*z)//in MPa
+sigma_st=m*sigma_cbc*(d-x)/x//in MPa
+mprintf("Stress in concrete=%f N/mm^2\nStress in tension steel=%f N/mm^2",sigma_cbc,sigma_st)