LaTeX.txt

    Variable      &      Value       \\
\midrule
      Mach Number &             2.82 \\
      Temperature & \SI{2925.27}{\K} \\
         Pressure & \SI{34.27}{\kPa} \\
Total Temperature & \SI{6649.83}{\K} \\
\bottomrule

 Variable   &         Value         \\
\midrule
Mach Number &                  3.82 \\
Temperature &      \SI{1492.64}{\K} \\
   Pressure &       \SI{2.14}{\kPa} \\
  Exit Area & \SI{2.51}{\m\squared} \\
     Thrust &     \SI{14573.61}{\N} \\
\bottomrule

  Species &          Concentration          &      Mass Fraction       \\
\midrule
\ce{C2H4} & \SI{0.00000}{\kmol\per\m\cubed} & \SI{0.00000}{\kg\per\kg} \\
\ce{  O2} & \SI{0.00021}{\kmol\per\m\cubed} & \SI{0.03876}{\kg\per\kg} \\
\ce{  CO} & \SI{0.00042}{\kmol\per\m\cubed} & \SI{0.06786}{\kg\per\kg} \\
\ce{ H2O} & \SI{0.00079}{\kmol\per\m\cubed} & \SI{0.08188}{\kg\per\kg} \\
\ce{ CO2} & \SI{0.00037}{\kmol\per\m\cubed} & \SI{0.09340}{\kg\per\kg} \\
\ce{  N2} & \SI{0.00445}{\kmol\per\m\cubed} & \SI{0.71810}{\kg\per\kg} \\
\bottomrule