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authorprashantsinalkar2018-02-03 11:01:52 +0530
committerprashantsinalkar2018-02-03 11:01:52 +0530
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parentd1e070fe2d77c8e7f6ba4b0c57b1b42e26349059 (diff)
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+clear
+//
+//
+
+//Given
+//Variable declaration
+b=200 //Width in mm
+d=300 //Depth in mm
+L=5*1000 //Span in mm
+L_star=5 //Span in m
+w=9*1000 //Uniformly distributed load in N/m
+E=1e4 //Youngs modulus in N/sq.mm
+
+//Calculation
+W=w*L_star //Total load in N
+I=b*d**3/12 //Moment of Inertia in mm^4
+
+//case(i):the slope at the support
+thetaA=(-(W*(L**2))/(24*E*I))
+
+
+//case(ii):maximum deflection
+yc=(W*L**3)/(E*I)*(5/384)
+
+//Result
+printf("\n Slope at the support = %0.3f radians",-thetaA)
+printf("\n Maximum deflection = %0.3f mm",yc)