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Overhanging Beam - Uniformly Distributed Load Overhanging Both Supports

ob 4A

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.

 

Overhanging Beam - Uniformly Distributed Load Overhang Both Supports formulas

\( R_1 \;=\;  \dfrac{  w\cdot L \cdot ( L - 2 \cdot c )  }{ 2 \cdot b  }    \) 

\( R_2 \;=\;   \dfrac{  w\cdot L \cdot ( L - 2 \cdot a )   }{ 2 \cdot b  }  \) 

\( V_1  \;=\;   w\cdot a   \) 

\( V_2  \;=\;   R_1 - V_1   \)

\( V_3  \;=\;   R_2 - V_4   \)

\( V_4  \;=\;   w\cdot c   \)

\( V_{x_1}  \;=\;   V_1 -  (\; w \cdot ( a - x_1 ) \;)  \)

\( V_x \; ( x < b )   \;=\;   R_1 - (\; w \cdot ( a + x ) \;)   \)

\( M_1 \;=\;     - \;  \dfrac{ w\cdot a^2 }{ 2 }    \)

\( M_2 \;=\;  - \;  \dfrac{ w \cdot c^2 }{ 2  }  \)

\( M_3 \;\;=\;\;   R_1 \cdot  \left(  \dfrac{ R_1 }{ 2\cdot w } - a  \right)  \)

\( M_x \;=\;      R_1 \cdot x \cdot -\; \dfrac{ w \cdot ( a + x )^2 }{ 2 }     \)

Symbol English Metric
\( x \) = 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 \(in\) \(mm\)
\( a, b, c \) = span length under consideration \(in\) \(mm\)

 

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