Q1: Mass flow through a sonic nozzle is a function of gas pressure and temperature(Pressure = P, Temperature = T). If the mass flow rate through the nozzle is given by:Pm = 0.0430;Where: m Ib/min, P = Psia, T= "RTO.5a) Determine what the units for the constant 0.0430 are?b) What will be the new value of the constant, now gives as 0.0430, if the variables in theequation are to be substituted with SI units and m is cakulated in SI units?

GIVEN: mass flow rate through the nozzle m =0.430pT0.5 here m = mass flow Ib/ min P = pressure…

Q1: Mass flow through a sonic nozzle is a function of gas pressure and temperature (Pressure = P, Temperature = T). If the mass flow rate through the nozzle is given by: m = 0.0430 0 Where: m lb/min, P Psia, T "R a) Determine what the units for the constant 0.0430 are? b) What will be the new value of the constant, now gives as 0.0430, if the variables in the equation are to be substituted with SI units and m is calculated in SI units?

Q1: Mass flow through a sonic nozzle is a function of gas pressure and temperature (Pressure = P, Temperature = T). If the mass flow rate through the nozzle is given by: m = 0.0430 0 Where: m lb/min, P Psia, T "R a) Determine what the units for the constant 0.0430 are? b) What will be the new value of the constant, now gives as 0.0430, if the variables in the equation are to be substituted with SI units and m is calculated in SI units?

College Physics

10th Edition

ISBN:9781285737027

Author:Raymond A. Serway, Chris Vuille

Publisher:Raymond A. Serway, Chris Vuille

Chapter9: Solids And Fluids

Section: Chapter Questions

Problem 2CQ: The density of air is 1.3 kg/m3 at sea level. From your knowledge of air pressure at ground level,...

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