{
  "rows": 5050,
  "source": "https://web.mit.edu/16.unified/www/SPRING/propulsion/notes/node131.html",
  "constants": {
    "cp_J_kgK": 4200.0,
    "UA_W_K": 10.0,
    "inlet_C": 20.0,
    "wall_C": 80.0
  },
  "model": "T(s)=Tw+(Tin-Tw)exp[-UA*s/(mdot*cp)]",
  "verification": {
    "RK4_100_segments_max_outlet_error_K": 3.608346332839574e-08
  },
  "limits": [
    "Constant wall temperature and conductance, independent of flow rate in this comparison.",
    "No phase change, axial conduction, pressure drop, entrance effects or heater control.",
    "A colder outlet at larger mass flow does not necessarily mean a lower total heat-transfer rate."
  ]
}