$\backslash$table$[[$Ambient pressure:,$p_{\text{a}\text{m}\text{b}}$ :$=1$ bar,$],[$Inlet temperature:,$t_1$:$=15,C,],[$Intake loss factor:,${}_{in}$:$=0\mathrm{.}96,],[$Pressure ratio of the compressor:,r$.$:$=28,],[$Efficiency of the compressor:,${}_c$:$=0\mathrm{.}85,],[$Heating value of the fuel:,$H$:$=42000k\frac{J}{k}g,],[$Combustion chamber loss factor:,r$.{}_{cc}$:$=0\mathrm{.}95,],[$Turbine inlet temperature:,$t3$:$=1400C,],[$Efficiency of the turbine:,${}_t$:$=0\mathrm{.}9,],[$Exhaust loss factor.,${}_{\text{o}\text{u}\text{t}}$:$=0\mathrm{.}94,],[$Mass flow rate of air:,$m_{\text{a}\text{i}\text{r}}$:$=10,k\frac{g}{s},{}_{\text{a}\text{i}\text{r}}$:$=1\mathrm{.}25k\frac{g}{m^3}$

What formulas should I use to calculate these data