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Simple Beam - Uniform Load Partially Distributed at One End

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.

 

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Simple Beam - Uniform Load Partially Distributed at One End formulas

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

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

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

\( M_{max} \; ( at \; x \;=\; R_1\;/\;w )  \;=\;  \dfrac{ R_{1}{^2} }{ 2 \cdot w  }\)

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

\( M_x \; (  x > a )  \;=\;   R_2  \cdot (  L - x )  \)

\( \Delta_x  \; (  x < a )  \;=\;    \dfrac{ w\cdot x }{ 24 \cdot \lambda \cdot I \cdot L }   \cdot   [\; (\; a^2  \cdot ( 2 \cdot L - a )^2\;) - (\; 2 \cdot a \cdot x^2 \cdot (  2 \cdot L - a )\;)  + L \cdot x^3  \;]    \)

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

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 \(in\) \(mm\)
\( w \) = load per unit length \(lbf\;/\;in\) \(N\;/\;m\)
\( a \) = width of UDL \(in\) \(mm\)
\( L \) = span length of the bending member \(in\) \(mm\)
\( x \) = horizontal distance from reaction to point on beam \(in\) \(mm\)
\( \lambda  \)   (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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