When a simply-supported elastic beam of span $L$ and flexural rigidity $EI$ is loaded with a uniformly distributed load $w$ per unit length, the deflection at the mid-span is \[ \Delta_0=\frac{5}{384}\,\frac{wL^4}{EI}. \] If the load on one half of the span is now removed, the mid-span deflection
Step 1: Use superposition.
Write the full UDL as the sum of two half-span UDLs: one on $[0,L/2]$ and one on $[L/2,L]$.
Let $\delta_{\text{half}}$ be the mid-span deflection when only one half is loaded (either left or right).
Step 2: Exploit symmetry at mid-span.
The mid-span deflection from loading the left half equals that from loading the right half (by symmetry).
Hence, the full UDL mid-span deflection is
\[
\Delta_0=\delta_{\text{half}}+\delta_{\text{half}}=2\,\delta_{\text{half}}.
\]
Step 3: Conclude for the new loading.
With only one half loaded, the mid-span deflection is
\[
\delta_{\text{half}}=\frac{\Delta_0}{2}
=\frac{1}{2}\left(\frac{5}{384}\frac{wL^4}{EI}\right)
=\frac{5}{768}\frac{wL^4}{EI}.
\]
Therefore, it reduces to $\Delta_0/2$.
\[
\boxed{\delta_{\text{mid (half UDL)}}=\Delta_0/2}
\]
A 2D thin plate (plane stress) has $E=1.0~\text{N/m}^2$ and Poisson’s ratio $\mu=0.5$. The displacement field is $u=Cx^2y$, $v=0$ (in m). Distances $x,y$ are in m. The stresses are $\sigma_{xx}=40xy~\text{N/m}^2$ and $\tau_{xy}=\alpha x^2~\text{N/m}^2$. Find $\alpha$ (in $\text{N/m}^4$, integer).
The infinitesimal element shown in the figure (not to scale) represents the state of stress at a point in a body. What is the magnitude of the maximum principal stress (in N/mm², in integer) at the point?

| Point | Staff Readings Back side | Staff Readings Fore side | Remarks |
|---|---|---|---|
| P | -2.050 | - | 200.000 |
| Q | 1.050 | 0.95 | Change Point |
| R | - | -1.655 | - |