- #1
optrix
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I wasn't sure whether to put this in Aerospace, but decided on physics in the end.
1.) How do you factor a chemical reaction into the solution for the Navier Stokes equations? More precisely, how can you include the affects of a heat absorbing (endothermic), or heat releasing (exothermic) chemical reaction going in within the flow field? The main thing I have in mind is combustion reactions that occur in jet engines, which are of course exothermic.
My thoughts were that you would first have to calculate the enthalpy of combustion of the fuel. Then the amount of heat being released is related to the reaction rate, which depends on pressure, and density of air/fuel at a given point (Maybe even "concentration" is a better word). But then in turn, the amount of heat being released would affect the thermal expansion of the gas, and hence the pressure at that point, which again would change the reaction rate and amount of heat being released...etc... until maybe it reaches some kind of equilibrium?
I was also thinking that you would have to use scalar fields of the form f(x,t) for reaction rate and temperature. Would this be accurate?
2.) A related question - kerosene is made up of a whole mixture of hydrocarbons, and other things.
i. where can I find a list of the exact chemical compostion of kerosene? (I believe it may come in different 'grades' or classes, like A1, A2.)
ii. can you consider kerosene to be a uniform mixture of its constituent compounds, and therefore asign to it an overall enthalpy of combustion, which is like an average for all the constituents?
I'm having a lot of trouble finding information on any of these things, so if anyone knows then please help me out. (Number 1 is the main concern, but though I might as well drop number 2 in there too :) )
Appreciate any help, regards, Joe
1.) How do you factor a chemical reaction into the solution for the Navier Stokes equations? More precisely, how can you include the affects of a heat absorbing (endothermic), or heat releasing (exothermic) chemical reaction going in within the flow field? The main thing I have in mind is combustion reactions that occur in jet engines, which are of course exothermic.
My thoughts were that you would first have to calculate the enthalpy of combustion of the fuel. Then the amount of heat being released is related to the reaction rate, which depends on pressure, and density of air/fuel at a given point (Maybe even "concentration" is a better word). But then in turn, the amount of heat being released would affect the thermal expansion of the gas, and hence the pressure at that point, which again would change the reaction rate and amount of heat being released...etc... until maybe it reaches some kind of equilibrium?
I was also thinking that you would have to use scalar fields of the form f(x,t) for reaction rate and temperature. Would this be accurate?
2.) A related question - kerosene is made up of a whole mixture of hydrocarbons, and other things.
i. where can I find a list of the exact chemical compostion of kerosene? (I believe it may come in different 'grades' or classes, like A1, A2.)
ii. can you consider kerosene to be a uniform mixture of its constituent compounds, and therefore asign to it an overall enthalpy of combustion, which is like an average for all the constituents?
I'm having a lot of trouble finding information on any of these things, so if anyone knows then please help me out. (Number 1 is the main concern, but though I might as well drop number 2 in there too :) )
Appreciate any help, regards, Joe