## 5 Conclusions
\begin{table}
\begin{tabular}{c c c c} \hline \hline
**Uncertainty Source** & **Symbol** & **Value, \%** & **Note** \\ \hline Total pressure & \(q_{1}\) & 0.025 & Atmospheric air pressure measured by the air-data sensing system onboard \\ \hline Mach number & \(q_{2}\) & 1.01 & Obtained by the air-data sensing system onboard \\ \hline Pitot measurement & \(q_{3}\) & 3.5 & Max. percent uncertainty obtained as 1\(\sigma\) over an averaged value for 1-min duration for all probes \\ \hline Response surface methodology & \(q_{4}\) & 1.8 & Uncertainty obtained from Figure 10, including pitot pressure measurement error \\ (RSM) (Interpolation) & \(q_{4}\) & 4.1 (4.06) & Total uncertainty and corresponding to \(\varepsilon\) in Equation (9) \\ \hline \hline \end{tabular}
\end{table} 
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