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Simple Beam - Central Point Load and Variable End Moments

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.

 

sb 13D

Simple Beam - Central Point Load and Variable End Moments formulas

\( R_1 \;=\; V_1  \;=\; \dfrac{ P }{ 2 }  +  \dfrac{ M_1 - M_2 }{ L } \)
 

\( R_2 \;=\; V_2  \;=\; \dfrac{ P }{ 2 }  -  \dfrac{ M_1 - M_2 }{ L } \) 

\( M_3 \; (at\; center )  \;=\; \dfrac{ P \cdot L }{ 4 }  -  \dfrac{ M_1 + M_2 }{ L }  \) 

\( M_x \; ( x <  \frac{L}{2}  )  \;=\;  \left(\; \dfrac{ P }{ 2} + \dfrac{ M_1 - M_2 }{ L } \cdot x \;\right) - M_1  \)

\( M_x \; ( > \frac{L}{2} )  \;=\;  \left( \dfrac{ P}{2} \cdot ( L - x ) \right) +   \left( \dfrac{ ( M_1 - M_2 ) \cdot x }{ L } \right) - M_1    \)

\( \Delta_x  ( x <  \frac{L}{2} )  \;=\;  \dfrac{ P\cdot x }{ 48\cdot \lambda\cdot I }    \cdot                     \left(\;   3\cdot L^2 - 4\cdot x^2   -  \dfrac{ 8\cdot ( L - x ) }{ P\cdot L }  \cdot ( \;M_1 \cdot ( 2\cdot L - x ) + M_2\cdot ( L + x ) \; )             \;\right)  \)

\( x \; (first \;point \;of \;contraflexure ) \;=\;  \dfrac{ 2 \cdot L\cdot M_1 }{ L\cdot P + 2\cdot M_1 - 2\cdot M_2  } \)

\( x \; (second\; point \;of\; contraflexure ) \;=\; \dfrac{  L \cdot ( L\cdot P - 2\cdot M_1 )  }{ L\cdot P - 2\cdot M_1 + 2\cdot M_2  } \)

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

 

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