JuanMC
Mechanical
- Dec 20, 2006
- 20
I have a heat exchanger, (shell & tubes) fan-cooled. It cools oil from 55 °C to 45°C. I would like to increase the net heat transfer with the minimum changes in the system. I have determined the additional heat stream that i need, but don't know how to relate it with the heat exchanger. This is what i've done:
1. I made tests and with Heat = mass flow x Cp x (Thout - Thin), i got the net heat transfer rate.
2. With this, applying LMTD (and F), I got the UA coefficient.
The problem is that the UA is the inverse of the thermal resistance of the system: it depends of the conductive and convection coefficients. The first one is related with the material of the tubes and the second, with the fluid's characteristics: viscosity, density, type of flow, but NOT temperature.
There is a way to decrease the air temperature, but first, i need to get how much would that help me.
I've tried to calculate it in the next way:
1. With the expermimental heat transfer, I got the UA (said before)
2. With UA, and different air temperatures, i calculate (again) the heat transfer rate (it is different of the inicial, due to the correction factor for cross flow exchangers)
3. Also, i get a new heat transfer rate. So, i calculate the "real" temperature for oil at the exit, loosing this heat.
4. Finally, i calculate the total heat lost by the oil with this "real" temperature.
5. I start again the process, until both values are the same.
I'll appreciate any help. I don't know if what i've done is ok.
Thanks!
1. I made tests and with Heat = mass flow x Cp x (Thout - Thin), i got the net heat transfer rate.
2. With this, applying LMTD (and F), I got the UA coefficient.
The problem is that the UA is the inverse of the thermal resistance of the system: it depends of the conductive and convection coefficients. The first one is related with the material of the tubes and the second, with the fluid's characteristics: viscosity, density, type of flow, but NOT temperature.
There is a way to decrease the air temperature, but first, i need to get how much would that help me.
I've tried to calculate it in the next way:
1. With the expermimental heat transfer, I got the UA (said before)
2. With UA, and different air temperatures, i calculate (again) the heat transfer rate (it is different of the inicial, due to the correction factor for cross flow exchangers)
3. Also, i get a new heat transfer rate. So, i calculate the "real" temperature for oil at the exit, loosing this heat.
4. Finally, i calculate the total heat lost by the oil with this "real" temperature.
5. I start again the process, until both values are the same.
I'll appreciate any help. I don't know if what i've done is ok.
Thanks!