Step 1: Recall the formulas for Hoop Stress and Longitudinal Stress in a thin cylindrical shell.
For a thin cylindrical shell subjected to an internal pressure \( P \), with radius \( R \) and thickness \( t \):
The Hoop Stress (circumferential stress), \( \sigma_h \), is given by:
\[
\sigma_h = \frac{PR}{t}
\]
The Longitudinal Stress (axial stress), \( \sigma_l \), is given by:
\[
\sigma_l = \frac{PR}{2t}
\]
Step 2: Analyze the effect of increasing radius and thickness by 10%.
Let the original radius be \( R \) and the original thickness be \( t \).
The new radius, \( R' \), is increased by 10%:
\[
R' = R + 0.10R = 1.1R
\]
The new thickness, \( t' \), is increased by 10 %:
\[
t' = t + 0.10t = 1.1t
\]
The internal pressure \( P \) is assumed to remain constant.
Step 3: Calculate the new Hoop Stress (\( \sigma_h' \)).
Substitute \( R' \) and \( t' \) into the formula for hoop stress:
\[
\sigma_h' = \frac{P R'}{t'} = \frac{P (1.1R)}{(1.1t)}
\]
\[
\sigma_h' = \frac{1.1PR}{1.1t} = \frac{PR}{t}
\]
Since \( \sigma_h = \frac{PR}{t} \), we have \( \sigma_h' = \sigma_h \).
Step 4: Calculate the new Longitudinal Stress (\( \sigma_l' \)).
Substitute \( R' \) and \( t' \) into the formula for longitudinal stress:
\[
\sigma_l' = \frac{P R'}{2t'} = \frac{P (1.1R)}{2(1.1t)}
\]
\[
\sigma_l' = \frac{1.1PR}{2.2t} = \frac{PR}{2t}
\]
Since \( \sigma_l = \frac{PR}{2t} \), we have \( \sigma_l' = \sigma_l \).
Step 5: Determine the percentage increase in stresses.
Percentage increase in Hoop Stress:
\[
\text{Percentage Increase} = \frac{\sigma_h' - \sigma_h}{\sigma_h} \times 100% = \frac{\sigma_h - \sigma_h}{\sigma_h} \times 100% = 0%
\]
Percentage increase in Longitudinal Stress:
\[
\text{Percentage Increase} = \frac{\sigma_l' - \sigma_l}{\sigma_l} \times 100% = \frac{\sigma_l - \sigma_l}{\sigma_l} \times 100% = 0%
\]
Therefore, both the hoop stress and longitudinal stress remain unchanged. The increase in percentage for both is 0%.
The final answer is $\boxed{\text{2}}$.