| Inlet Input | Description |
| Flow In | Flow Data Input, 25x1 vector consisting of:
-1- W - gas path flow [pps] -2- s - entropy [BTU/(lbm*degR)] -3- Tt - total temperature [degR] -4- Pt - total pressure [psia] -5- ht - total enthlapy [BTU/lbm] -6- rhot - total density [lbm/ft3] -7- gamt - total specific heat ratio -8- Ts - static temperature [degR] -9- Ps - static pressure [psia] -10- hs - static enthalpy [BTU/lbm] -11- rhos - static density [lbm/ft3] -12- gams - static specific heat ratio -13- Vflow - flow velocity [ft/sec] -14- MN - Mach number -15- A - flow area [in2] -16to21- species array values, defined in canteraload.m -22to25- future use |
| Inlet Output | Description |
| Flow Out | Flow Data Output, 25x1 vector consisting of:
-1- W - gas path flow [pps] -2- Tt - total temperature [degR] -3- Pt - total pressure [psia] -4- ht - total enthlapy [BTU/lbm] -5to10- species array values, defined in canteraload.m -11- s - entropy [BTU/(lbm*degR)] -12- rhot - total density [lbm/ft3] -13- Ts - static temperature [degR] -14- Ps - static pressure [psia] -15- hs - static enthalpy [BTU/lbm] -16- rhos - static density [lbm/ft3] -17- Vflow - flow velocity [ft/sec] -18- MNin - Mach number -19- A - flow area [in2] -20- gamt - total specific heat ratio -21- gams - static specific heat ratio -22to25- future use |
| I_Data | Inlet additional calculation Data |
| Inlet Mask Variable | Description |
| recovery_M | pressure recovery [frac] |