Hi all,
Hoping that someone may be able to push me in the right direction. I'm attempting to perform design calculations for a simple and small shell & tube heat exchanger, for an academic project (simple in the sense of excluding calculations relating to nozzles, front/rear heads etc). However I have faced an issue regarding exceedingly large pressure drop across my baffle windows.
Pressure drop accounting for cross flow and end zone is approximately 10kPa (reasonable), however the pressure drop across the baffle windows is calculated as 249kPa- much too high. I can't understand why it's such a large drop through the windows, and how I can reduce this?
I increased the baffle spacing to reduce the number of baffles and increase the crossflow area, and I also increased the baffle cut to reduce the velocity through the windows. These geometrical variations have allowed me to reduce the window pressure drop to 144kPa, which is a good reduction, but still too high.
Can anyone provide advice on how to reduce this further without impacting the heat transfer coefficient too greatly? I have no experience in heat exchanger design, and most of what I have learnt is from Heat Exchanger Design Handbook (VDI-Verlag GmbH) and Coulson & Richardson's Chemical Engineering Design, so I am unsure if I am missing some fundamental principles when it comes to geometry ratios? Otherwise, the issue could potentially lie with my fluid input parameters (which can also be altered but I want to avoid phase-change).
The current design has a 20% heat transfer area over-design, so I do have some wiggle-room in terms of impacting the heat transfer coefficient. I have also attached my design calculator (sheet titled "Numerical"), if you wish to view the current input parameters (rows 6-16). Apologies for its state, it was never my intention to share the calculator.
Calcs #3 - S- 290, T- 20.xlsx 42.11KB
11 downloads
Any contributions would be well and truly appreciated.
Sincerely -
a mechanical engineering student who is in way over their head, but recognizes it's too late to turn back now