Step 1: List all variables and their dimensions.
$V \to LT^{-1}$, $\rho \to ML^{-3}$, $\mu \to ML^{-1}T^{-1}$, $c \to L$, and $\alpha$ is already dimensionless (a ratio/angle).
Step 2: Form the dimensionless group from the dimensional variables using the exponent method.
Look for a combination $\rho^a V^b c^d \mu^{-1}$ that is dimensionless. Matching mass: $a = 1$. Matching time: from $\mu^{-1}$ giving $+1$ power of $T$, and $V^b$ giving $-b$, balance gives $b=1$. Matching length: $-3a + b + d + 1 = 0 \Rightarrow -3+1+d+1=0 \Rightarrow d=1$. So the group is
\[ \Pi_1 = \frac{\rho V c}{\mu} = Re \]
This confirms, from first principles rather than by counting, that the 4 dimensional quantities $V, \rho, \mu, c$ collapse into exactly one dimensionless number.
Step 3: Bring back the parameter that was already dimensionless.
$\alpha$ never needed reduction, so it stands on its own as a second independent parameter, $\Pi_2 = \alpha$. The full aerodynamic response (lift, drag, pressure distribution) at low Reynolds number depends only on the pair $(\Pi_1, \Pi_2) = (Re, \alpha)$.
Step 4: Size a full factorial test grid over the two parameters.
A full factorial design that sweeps 10 equally spaced levels of $Re$ against 10 equally spaced levels of $\alpha$ needs one run for every combination:
\[ N_{min} = 10 \times 10 = 100 \]
Step 5: Sanity check against the wrong options.
If someone forgot to combine $V, \rho, \mu, c$ into $Re$ first, they would think there are 5 raw parameters and plan $10^5 = 1,00,000$ runs (option D), or 4 raw parameters giving $10^4=10,000$ runs (option C); both waste effort because many of those raw combinations repeat the same $Re$. Treating everything as one parameter (option A, 10 runs) under-samples, since $\alpha$ genuinely changes the flow independently of $Re$ and must be swept separately.
Only the reduced pair $(Re, \alpha)$ gives the true minimum.
\[ \boxed{N_{min} = 100} \]