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Overhanging Beam - Uniformly Distributed Load

Diagram Symbols

Bending moment diagram (BMD)  -  Used to determine the bending moment at a given point of a structural element.  The diagram can help determine the type, size, and material of a member in a structure so that a given set of loads can be supported without structural failure.
Free body diagram (FBD)  -  Used to visualize the applied forces, moments, and resulting reactions on a structure in a given condition.
Shear force diagram (SFD)  -  Used to determine the shear force at a given point of a structural element.  The diagram can help determine the type, size, and material of a member in a structure so that a given set of loads can be supported without structural failure.
Uniformly distributed load (UDL)  -  A load that is distributed evenly across the entire length of the support area.

 

ob 1A

Overhanging Beam - Uniformly Distributed Load formulas

\( R_1 \;=\; V_1 \;=\;    \dfrac{ w }{ 2 \cdot L }  \cdot  (L^2 - a^2)   \) 

\( R_2 \;=\; V_2 + V_3 \;=\;   \dfrac{ w }{ 2 \cdot L } \cdot  ( L + a )^2  \) 

\(V_2  \;=\;   w \cdot a  \) 

\( V_3  \;=\;    \dfrac{ w }{ 2 \cdot L }  \cdot  (L^2 + a^2)   \)

\( V_x  \; (between\; supports )  \;=\;     R_1 - w \cdot x  \)

\(V_{x_1} \; (for \;overhang )  \;=\;    w \cdot  ( a - x_1 )  \)

\( M_x  \; (between\; supports )  \;=\;  \dfrac{ w\cdot x }{ 2 \cdot L } \cdot ( L^2 - a^2 - x\cdot L )    \)

\( M_{x_1} \; (overhang )  \;=\;  \dfrac{ w }{ 2 } \cdot  ( a - x_1 )^2    \)

\( M_1  \; [\;at\;  x = \frac{L}{2}  (1 - \frac{ a^2}{L^2} )\;] \;=\;   \dfrac{ w }{ 8\cdot L^2 } \; (L + a)^2 \cdot (L - a)^2  \)

\( M_2 \; (at\; R_2 )  \;=\;  \dfrac{ w\cdot a^2 }{ 2 }  \)

\( \Delta_x  \; (between \;supports ) \;=\;   \dfrac{ w \cdot x }{ 24 \cdot \lambda \cdot I \cdot L }  \cdot   ( L^4  - 2\cdot L^2\cdot x^2  + L\cdot x^3  - 2\cdot a^2\cdot L^2 + 2\cdot a^2\cdot x^2 )    \)

\( \Delta_{x_1}  \; (for\; overhang )  \;=\;   \dfrac{ w\cdot x_1 }{ 24 \cdot \lambda \cdot I }  \cdot    ( 4\cdot a^2\cdot L  - L^3  + 6\cdot a^2\cdot x_1 - 4\cdot a\cdot x_{1}{^2} +  x_{1}{^3} )    \)

Symbol English Metric
\( \Delta \) = deflection or deformation \(in\) \(mm\)
\( x \) = horizontal distance from reaction to point on beam \(in\) \(mm\)
\( w \) = load per unit length \(lbf\;/\;in\) \(N\;/\;m\)
\( M \) = maximum bending moment \(lbf-in\) \(N-mm\)
\( V \) = maximum shear force \(lbf\) \(N\)
\( \lambda  \)   (Greek symbol lambda) = modulus of elasticity \(lbf\;/\;in^2\) \(Pa\)
\( R \) = reaction load at bearing point \(lbf\) \(N\)
\( I \) = second moment of area (moment of inertia) \(in^4\) \(mm^4\)
\( L \) = span length of the bending member \(in\) \(mm\)

 

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