Step 1: Use the expression for logarithmic decrement.
For an underdamped single degree of freedom system, the logarithmic decrement is related to the damping ratio by:
\[ \delta = \frac{2\pi \zeta}{\sqrt{1-\zeta^2}} \]
Here, $\zeta$ represents the damping ratio of the system.
Step 2: Insert the given damping ratio.
The damping ratio is specified as:
\[ \zeta = 0.01 \]
Since the damping is very small, the denominator is approximately equal to 1, giving:
\[ \delta \approx 2\pi \times 0.01 = 0.0628 \]
Step 3: Determine amplitude change after three cycles.
The ratio of the amplitude after $n$ cycles to the initial amplitude is given by:
\[ \frac{x_n}{x_0} = e^{-n\delta} \]
For three successive cycles:
\[ \frac{x_3}{x_0} = e^{-3 \times 0.0628} = e^{-0.1884} \approx 0.828 \]
Step 4: Compute the percentage decrease in amplitude.
The percentage reduction in peak amplitude is:
\[ (1 - 0.828) \times 100 = 17.2\% \]
Step 5: Final result.
\[ \boxed{17.2\%} \]
A pitot tube connected to a U-tube mercury manometer measures the speed of air flowing in the wind tunnel as shown in the figure below. The density of air is 1.23 kg m\(^{-3}\) while the density of water is 1000 kg m\(^{-3}\). For the manometer reading of \( h = 30 \) mm of mercury, the speed of air in the wind tunnel is _________ m s\(^{-1}\) (rounded off to 1 decimal place). 
Consider a velocity field \( \vec{V} = 3z \hat{i} + 0 \hat{j} + Cx \hat{k} \), where \( C \) is a constant. If the flow is irrotational, the value of \( C \) is (rounded off to 1 decimal place).