Tea break finished!
Now that we know the steam velocity at the exit of the nozzle, the specific volume of the steam and the mass flow, we can calculate the area and hence the nozzle exit diameter:
0.75bar absolute nozzle exit diameter = 2.46mm
0.5bar absolute nozzle exit diameter = 2.90mm
In a similar way we can calculate the throat diameter of the nozzle; although in this case the results are independent of the output steam pressure. There is no point in the steam pressure at the throat of the nozzle being below the critical pressure, as we will not get any advantage in terms of mass flow. So the pressure at the throat is taken as 0.58 times the input pressure, ie, 7.39bar absolute. From the Mollier chart we get a dryness fraction of 96%, and can then calculate the specific volume of 0.249m³/kg and an enthalpy of 2683300J/kg for the steam at the throat. In both cases the change in enthalpy is 103090J/Kg. The steam velocity at the throat is calculated in the same way as for the exit steam, except that the frictional losses are taken to be zero. For both cases we get a steam velocity of 454m/s; in rough terms a bit less the speed of sound in steam at the throat pressure. Similarly we can use the mass flow rate to calculate the throat area, and hence diameter to get 1.29mm. To summarise:
Output steam pressure = 0.75bar absolute nozzle exit diameter = 2.46mm nozzle throat diameter = 1.29mm
Output steam pressure = 0.5bar absolute nozzle exit diameter = 2.90mm nozzle throat diameter = 1.29mm
A further question arises as to the shape of the convergent and divergent parts of the steam nozzle. Here the ME words of wisdom and the professionals diverge (pun intended).
For the convergent part of the nozzle it doesn't really matter as long as the transitions are smooth and the recommendations in the professional literature is to keep it short. One publication mentions a length of 6mm; this for large nozzles with flow rates two orders of magnitude larger than my injector. The concept is discussed in the book by Crawford, and given the barest of mentions in the book by Brown. Both then go onto to use relatively shallow tapers. I plan to use a fairly short trumpet shaped convergent cone. Since the convegent part of the cone is short, and the steam velocity is subsonic, the frictional losses can be conveniently ignored.
For the divergent part of the nozzle again the actual angle isn't that important. Too shallow and the nozzle will be overly long with attendant frictional losses. Too steep and the steam may not be able to expand quickly enough, leading to turbulence. Values of around 10º included are discussed in the professional literature. This ties in well with practical ME injectors, where 9º seems to be a de facto value.
Given that the nozzle exit and throat diameters are calculated based on a series of idealised assumptions, and an estimate of frictional losses I don't think that they need to be particularly accurate in themselves.
Now that I have values for the nozzle exit and throat diameters the next phase of the investigation will look at the performance as the input pressure decreases to try and estimate the range over which the injector may work. I will also be looking at the kinetic energy and momentum available at various input pressures.
Andrew