Given:
Atmospheric pressure head \( H_a = 9 \, \text{m} \)
Vapour pressure head \( H_v = 1 \, \text{m} \)
Failure (total) head \( H = 40 \, \text{m} \)
Cavitation coefficient \( \sigma = 0.15 \)
The safe height \( h \) above tailrace level is given by:
\[
\sigma = \frac{H_a - H_v - h}{H}
\]
Substitute known values:
\[
0.15 = \frac{9 - 1 - h}{40}
\]
\[
0.15 \times 40 = 8 - h
\]
\[
6 = 8 - h
⇒ h = 8 - 6 = 2 \, \text{m}
\]
\[
\boxed{h = 2 \, \text{m}}
\]