Subject : Structural Analysis 1

Topic : Deflection of Beams

Difficulty : High

$1. Reaction:$

$\sum M_A=0$

$16*1+12*2-15-V_B*6=0$

$V_B=4.167KN$

$\sum F_Y=0$

$V_A-16-12+4.167=0$

$V_A=23.53KN$

$2. By \hspace{1mm} Macaulay's \int\int \hspace{1mm} integration \hspace{1mm} method:$

$Consider \hspace{1mm} part(xA)$

$B.M_x=EI\frac{d^2y}{dx^2}=4.167*x+15(x-2)^0-12(x-4)-8(x-4)\frac{(x-4)}{2}$

$\hspace{10mm} =4.167*x+15(x-2)^0-12(x-4)-4(x-4)^2 \hspace{1mm} eqn.1$

$Integrating \hspace{1mm} wrt \hspace{1mm} x$

$EI\frac{dy}{dx}=4.167*\frac{x^2}{2}+15(x-2)^1-\frac{12(x-4)^2}{2}-\frac{4(x-4)^3}{3}+C_1 \hspace{1mm} eqn.2 $

$EIy=4.167*\frac{x^3}{6}+\frac{15(x-2)^2}{2}-\frac{12(x-4)^3}{6}-\frac{4(x-4)^4}{12}+C_1x+C_2 \hspace{1mm} eqn.3 $

$3. Find \hspace{1mm} C_1 \hspace{1mm} and \hspace{1mm} C_2 \hspace{1mm}[Applying \hspace{1mm}boundary\hspace{1mm} …