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Simple Beam - Load Increasing Uniformly to 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 - Load Increasing Uniformly to One End formulas

\( R_1 \;=\ V_1 \;=\; \dfrac{ W }{ 3 }\)

\( R_2 \;=\ V_2 \;=\;  \dfrac{ 2 \cdot W }{3 }\)

\( V_x \;=\  \dfrac{ W }{ 3 }  -  \dfrac{ W \cdot x^2 }{ L^2 }\)

\( M_{max} \; (at \;  x = L\;/\; \sqrt{3}\; ) \;=\;  \dfrac{ 2 \cdot W \cdot L }{ 9\cdot \sqrt{3}   }\)

\( M_x \;=\;  \dfrac{ W \cdot x }{ 3 \cdot L^2 }  \cdot ( L^2  - x^2 )   \)

\( \Delta_{max} \; ( \;at \; x = L\; \sqrt{1 - ( 8/15 )^{\frac{1}{2} } } \;)  \;=\; 0.01304 \cdot  \dfrac{ W \cdot L^3 }{ \lambda \cdot I } \)

\( \Delta_x \;=\;  \dfrac{ W \cdot x }{ 180 \cdot \lambda \cdot I \cdot L^2 }  \cdot  ( 3 \cdot x^4 - 10 \cdot L^2 \cdot x^2 + 7 \cdot L^4 )  \)

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 \(in\) \(mm\)
\( W \) = total load or \( w\;L\;/\;2 \) \(lbf\) \(N\)
\( w \) = highest load per unit length of UIL \(lbf\;/\;in\) \(N\;/\;m\)
\( L \) = 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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