Sir,
Could you tell the way to derive the possible flow of Jet A1 fuel through a valve for same pressure drop (21kPa) when the maximum possible flow of air is 1400 lpm with the pressure drop of 21 kPa after that flow chocking has started which is clear from the steepness of the flow Vs pressure drop curve.
Will my flow rate of Jet A1 fuel will come down or it will increase compared to air?
Because, from the equation of friction loss, friction factor is directly proportional to kinematic viscosity of the fluid which is less for fuel compared to air. So the equation tells, for the same 21kPa, fuel flow rate will increase.