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Consistent load vector

A distributed load must be turned into forces at the nodes. The correct (consistent) way is to weight the load with the shape functions: Fie=∫Fx φi dxF^e_i = \int F_x\,\varphi_i\,dx. Then the nodal forces do the same work as the distributed load for every displacement the element can have.

Fe=qh2(11)F^e = \frac{qh}{2}\begin{pmatrix}1\\ 1\end{pmatrix}uniform load, linear element
Fe=h6(2q1+q2q1+2q2)F^e = \frac{h}{6}\begin{pmatrix}2q_1 + q_2\\ q_1 + 2q_2\end{pmatrix}linearly varying load
Fe=qh(1/62/31/6)F^e = qh\begin{pmatrix}1/6\\ 2/3\\ 1/6\end{pmatrix}uniform load, quadratic element

Symbols

qqdistributed loadN/m
hhelement lengthm
FieF^e_inodal forceN

Example

Load from q1=0q_1 = 0 to q2=6q_2 = 6 kN/m over h=3h = 3 m:

Fe=36(0+6, 0+12)=(3, 6)F^e = \frac36(0 + 6,\ 0 + 12) = (3,\ 6) kN. The sum 99 kN is the whole load 12⋅6⋅3\tfrac12\cdot 6\cdot 3.

Check: the sum of the nodal forces must always equal the whole load on the element.
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