Lecture 05 - Design and Simulation of Heat Exchangers

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Language: en

00:00:00.000
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00:00:14.250 00:00:14.260 this talk is about the design and
00:00:17.500 00:00:17.510 simulation of heat exchangers in
00:00:20.050 00:00:20.060 particular we want to do the LM TD
00:00:24.929 00:00:24.939 approach or the design of heat
00:00:28.450 00:00:28.460 exchangers by LM TD method so before
00:00:32.950 00:00:32.960 going into the details we want to look
00:00:35.260 00:00:35.270 into the design and simulation what do
00:00:38.710 00:00:38.720 we mean by design we want to see it with
00:00:42.369 00:00:42.379 the example of a counter-current heat
00:00:45.310 00:00:45.320 exchanger here this heat exchanger we
00:00:51.219 00:00:51.229 know what are the fluid streams the
00:00:54.130 00:00:54.140 process fluid streams or the process
00:00:56.290 00:00:56.300 parameters the inlet temperature the
00:00:58.810 00:00:58.820 exit temperature the exit and Inlet
00:01:01.539 00:01:01.549 pressure the flow rates all these
00:01:03.880 00:01:03.890 parameter process parameters are known
00:01:06.310 00:01:06.320 to us and what we want to find out is
00:01:09.910 00:01:09.920 the geometrical parameters like the
00:01:13.510 00:01:13.520 length the inner and outer diameter of
00:01:17.260 00:01:17.270 the tubes so in this counter current
00:01:21.910 00:01:21.920 heat exchanger what we are basically
00:01:24.219 00:01:24.229 trying to find out is the different
00:01:28.380 00:01:28.390 dimensions or the geometric geometrical
00:01:31.209 00:01:31.219 parameters or the dimensions of the heat
00:01:33.580 00:01:33.590 exchanger and we often call it as sizing
00:01:37.690 00:01:37.700 problem or the design problem because it
00:01:40.719 00:01:40.729 is related to the size of the heat
00:01:42.279 00:01:42.289 exchanger we call it sizing now in
00:01:45.669 00:01:45.679 contrast to this design we are also
00:01:49.749 00:01:49.759 often we know we try to solve the
00:01:52.149 00:01:52.159 simulation problem what is simulation in
00:01:55.989 00:01:55.999 simulation if we take the same heat
00:01:57.969 00:01:57.979 exchanger example that counter-current
00:02:00.489 00:02:00.499 heat exchanger in this case we know all
00:02:04.569 00:02:04.579 00:02:07.239 00:02:07.249 length of the exchanger the diameter
00:02:09.370 00:02:09.380 outer or inner all these parameters are
00:02:13.450 00:02:13.460 known in addition to that we also know
00:02:18.190 00:02:18.200 some of the process parameters like the
00:02:20.950 00:02:20.960 inlet fluid temperature
00:02:23.770 00:02:23.780 the flow rates are known that means we
00:02:27.460 00:02:27.470 know this fluid flow temperature we know
00:02:31.690 00:02:31.700 this Inlet temperature we know this
00:02:34.330 00:02:34.340 Inlet temperature and what we intend to
00:02:38.050 00:02:38.060 find out is the exit temperature of the
00:02:41.710 00:02:41.720 hot and cold fluid stream so this is
00:02:44.820 00:02:44.830 something related to the rating or the
00:02:54.240 00:02:54.250 simulation of the heat exchanger we call
00:02:57.580 00:02:57.590 it as simulation problem
00:03:08.250 00:03:08.260 so now we want to try the similar design
00:03:18.539 00:03:18.549 of a counter-current heat exchanger and
00:03:21.500 00:03:21.510 here this is an example we want to try
00:03:26.160 00:03:26.170 it with a counter-current heat exchanger
00:03:29.009 00:03:29.019 where we will assume a simple situation
00:03:33.809 00:03:33.819 by assuming C R or the C mean by C max
00:03:38.880 00:03:38.890 equals to 1 when we assume that she
00:03:42.750 00:03:42.760 recalls to 1 it will have a temperature
00:03:45.930 00:03:45.940 profile shown in the figure what we will
00:03:49.949 00:03:49.959 find that the delta T the temperature
00:03:54.150 00:03:54.160 difference between the hot and cold
00:03:56.309 00:03:56.319 fluid it will remain same throughout the
00:03:59.220 00:03:59.230 length of the heat exchanger so since we
00:04:03.569 00:04:03.579 are trying to solve a counter-current
00:04:06.000 00:04:06.010 heat exchanger design problem here the
00:04:09.569 00:04:09.579 fluid temperature the Inlet and outlet
00:04:12.740 00:04:12.750 all for the hot and cold fluids are
00:04:16.199 00:04:16.209 known here we have assumed C R equals to
00:04:20.789 00:04:20.799 1 now we want to find out what will be
00:04:24.029 00:04:24.039 the length or diameter of this heat
00:04:26.129 00:04:26.139 exchanger so what is C R it is basically
00:04:36.180 00:04:36.190 a ratio between the heat capacity of the
00:04:39.330 00:04:39.340 hot fluid and the cold fluid this CH or
00:04:44.010 00:04:44.020 the hot capacity ratio heat capacity is
00:04:49.620 00:04:49.630 basically a product of the hot fluid
00:04:53.339 00:04:53.349 specific heat multiplied by the mass
00:04:56.760 00:04:56.770 flow rate of the hot fluid and the cold
00:05:00.060 00:05:00.070 sea C or the cold capacity is equals to
00:05:03.990 00:05:04.000 a product of the specific heat of the
00:05:09.390 00:05:09.400 cold fluid multiplied by the mass flow
00:05:14.850 00:05:14.860 rate of the cold fluid so this 2 ratio
00:05:18.420 00:05:18.430 is basically
00:05:21.300 00:05:21.310 ratio between the hot and cold fluid is
00:05:23.920 00:05:23.930 equals to 1 we have assumed so in that
00:05:27.490 00:05:27.500 situation only we can expect this kind
00:05:30.130 00:05:30.140 of temperature profile now in this case
00:05:33.790 00:05:33.800 this is the hot in hot out and TC in and
00:05:38.470 00:05:38.480 TC out now if we take a small elemental
00:05:43.030 00:05:43.040 length DL across the length of the heat
00:05:46.360 00:05:46.370 exchanger we find that this is th and
00:05:51.580 00:05:51.590 this is TC and we also assume that the
00:05:55.720 00:05:55.730 internal temperature I mean the wall
00:05:57.820 00:05:57.830 temperature is T W so this TW is varying
00:06:02.560 00:06:02.570 from this end to this end now in
00:06:07.330 00:06:07.340 addition to this assumption that CR
00:06:11.140 00:06:11.150 equals to 1 that is the simplest case we
00:06:14.260 00:06:14.270 are making some more additional
00:06:16.030 00:06:16.040 assumptions like there is no external
00:06:19.090 00:06:19.100 heat in leak that means this fluid hot
00:06:22.870 00:06:22.880 fluid is not connected with the
00:06:24.550 00:06:24.560 environment neither this cold fluid is
00:06:27.310 00:06:27.320 connected with the environment the heat
00:06:30.250 00:06:30.260 is being supplied only from the hot
00:06:33.550 00:06:33.560 fluid to the cold fluid via this
00:06:36.520 00:06:36.530 separating wall the separating wall
00:06:41.680 00:06:41.690 thickness we are assuming it to be
00:06:44.410 00:06:44.420 negligible by saying that the wall
00:06:48.700 00:06:48.710 thickness is negligible we mean that the
00:06:52.960 00:06:52.970 heat flow from the hot fluid to the cold
00:06:55.300 00:06:55.310 fluid is not affected by the resistance
00:07:00.280 00:07:00.290 of the wall in addition to that we also
00:07:05.590 00:07:05.600 assume that there is no axial conduction
00:07:08.350 00:07:08.360 what is the actual conduction that it is
00:07:12.240 00:07:12.250 that this wall is having a kind of
00:07:15.400 00:07:15.410 temperature gradient but we are not
00:07:19.210 00:07:19.220 assuming any heat flowing from this end
00:07:22.930 00:07:22.940 of the wall to the other end only we are
00:07:25.750 00:07:25.760 assuming the heat flow from the hot
00:07:29.380 00:07:29.390 fluid to the cold fluid that's what is
00:07:32.920 00:07:32.930 the assumption actually
00:07:34.690 00:07:34.700 conduction heat is negligible so now
00:07:38.200 00:07:38.210 what will happen the hot fluid will give
00:07:42.880 00:07:42.890 heat to the separating wall the
00:07:46.390 00:07:46.400 separating wall in turn will give heat
00:07:49.180 00:07:49.190 to the cold fluid so how do we estimate
00:07:53.110 00:07:53.120 this heat transfer we will take the
00:07:56.890 00:07:56.900 difference between the hot fluid and the
00:08:00.220 00:08:00.230 wall so T H minus TW and The Associated
00:08:04.510 00:08:04.520 area with this fluid and the wall or the
00:08:09.430 00:08:09.440 hot side heat transfer surface area how
00:08:13.090 00:08:13.100 much is it that is say if it is a H then
00:08:18.520 00:08:18.530 we have considered only DL length of
00:08:22.840 00:08:22.850 this heat exchanger so if we assume that
00:08:27.580 00:08:27.590 the heat transfer surface area is
00:08:29.710 00:08:29.720 uniformly distributed over the entire
00:08:31.630 00:08:31.640 length we will find that the heat
00:08:38.830 00:08:38.840 transfer equation will look like
00:08:48.590 00:08:48.600 DQ is he calls to as I told you that it
00:08:53.910 00:08:53.920 is th minus TW and the area associated
00:08:58.590 00:08:58.600 with this elemental length DL that is H
00:09:04.139 00:09:04.149 by L and DL is the small element and
00:09:08.150 00:09:08.160 over an above HH the heat transfer
00:09:11.070 00:09:11.080 coefficient of the hot fluid side
00:09:12.889 00:09:12.899 similarly we can equate it to the heat
00:09:17.610 00:09:17.620 received from the wall to the cold fluid
00:09:20.280 00:09:20.290 and the related heat transfer surface
00:09:24.810 00:09:24.820 area and the heat transfer coefficient
00:09:27.199 00:09:27.209 corresponding to the cold fluid side now
00:09:35.510 00:09:35.520 if we simplify this equation or rather
00:09:41.340 00:09:41.350 if we integrate this equation over the
00:09:43.560 00:09:43.570 entire length we will find that this DQ
00:09:47.880 00:09:47.890 is becoming Q and this heat transfer
00:09:52.019 00:09:52.029 surface area is becoming a H so the
00:09:56.640 00:09:56.650 overall equation becomes H h H into T H
00:10:01.920 00:10:01.930 minus TW
00:10:02.910 00:10:02.920 and on this side TW minus TC and that
00:10:06.030 00:10:06.040 cold HC and AC now if we simplify this
00:10:11.040 00:10:11.050 equation to find out the wall
00:10:13.560 00:10:13.570 temperature we find this relation now
00:10:17.790 00:10:17.800 what we can do is that we can put this
00:10:21.210 00:10:21.220 wall temperature and replace it in
00:10:24.449 00:10:24.459 either of these equations when we
00:10:28.170 00:10:28.180 replace this equation or replace the
00:10:32.490 00:10:32.500 wall temperature to this equation the
00:10:37.110 00:10:37.120 earlier equation we find that the heat
00:10:40.650 00:10:40.660 transfer becomes this like this and if
00:10:44.850 00:10:44.860 we simplify this equation you will find
00:10:47.250 00:10:47.260 that this will look like HH h HC AC
00:10:54.420 00:10:54.430 divided by h HH HH CAC and the
00:10:59.430 00:10:59.440 difference between the wall temperature
00:11:00.920 00:11:00.930 this
00:11:02.100 00:11:02.110 nothing but delta T now when I take this
00:11:07.009 00:11:07.019 denominator and divide this part we find
00:11:11.550 00:11:11.560 this will be simplified like 1 by u a
00:11:14.970 00:11:14.980 equals to 1 by H h a h plus 1 by h CAC
00:11:21.590 00:11:21.600 that is nothing but the this part is the
00:11:27.329 00:11:27.339 hot fluid side heat transfer resistance
00:11:31.079 00:11:31.089 and this is the resistance offered by
00:11:33.960 00:11:33.970 the cold fluid side convective heat
00:11:36.690 00:11:36.700 transfer resistance and this one can be
00:11:39.540 00:11:39.550 represented by 1 by u way that is the
00:11:42.840 00:11:42.850 overall resistance offered by this fluid
00:11:47.519 00:11:47.529 so now this can be finally expressed in
00:11:52.470 00:11:52.480 the form of u way into delta T where
00:11:56.400 00:11:56.410 this delta T is the difference between
00:11:59.340 00:11:59.350 the two fluids and u way is the overall
00:12:03.389 00:12:03.399 heat transfer coefficient given by this
00:12:06.389 00:12:06.399 expression so if we now go to the next
00:12:17.550 00:12:17.560 slide
00:12:24.940 00:12:24.950 so in summary we can say that the Q is
00:12:30.430 00:12:30.440 given by you a delta T and so this is
00:12:37.569 00:12:37.579 the final outcome we have seen where you
00:12:41.829 00:12:41.839 a is given by 1 by a is related to the
00:12:45.850 00:12:45.860 individual heat transfer I mean
00:12:48.280 00:12:48.290 resistances offered by the cold and the
00:12:51.100 00:12:51.110 hot fluid and over an above we have this
00:12:56.069 00:12:56.079 individual mass balance for the hot and
00:12:59.379 00:12:59.389 the cold fluid the hot fluid mass
00:13:02.980 00:13:02.990 balance is given by CH and th in minus
00:13:07.750 00:13:07.760 th out similarly for the cold fluid we
00:13:11.230 00:13:11.240 can have this equation now as we are
00:13:15.790 00:13:15.800 trying to solve a design problem we know
00:13:19.110 00:13:19.120 the hot inlet we know the hot outlet we
00:13:23.680 00:13:23.690 know the cold inlet and the cold outlet
00:13:27.069 00:13:27.079 also so we know essentially the amount
00:13:31.449 00:13:31.459 of heat getting transferred so in this
00:13:34.180 00:13:34.190 equation we know Q we know the delta T
00:13:37.720 00:13:37.730 we have assumed a simple situation where
00:13:40.990 00:13:41.000 C R equals to 1 delta T is throughout
00:13:44.110 00:13:44.120 the length uniform so from this relation
00:13:48.100 00:13:48.110 we can calculate you way so this away
00:13:51.970 00:13:51.980 will now come to this equation where it
00:13:56.470 00:13:56.480 is the combination of 1 by H h a h and h
00:14:00.850 00:14:00.860 c AC now the hot side heat transfer
00:14:04.750 00:14:04.760 coefficient can also be obtained because
00:14:07.210 00:14:07.220 we know the mass flow rate h dot we can
00:14:13.240 00:14:13.250 also find out HC because the
00:14:16.720 00:14:16.730 corresponding mass flow rate is also
00:14:20.290 00:14:20.300 known MC dot is also known we can also
00:14:24.280 00:14:24.290 try to find out this HC and then we can
00:14:30.040 00:14:30.050 try to find out the a H and AC but this
00:14:35.050 00:14:35.060 is only one equation where the number of
00:14:37.990 00:14:38.000 unknowns
00:14:38.980 00:14:38.990 many like the length internal diameter
00:14:44.910 00:14:44.920 outside diameter so in order to find out
00:14:48.540 00:14:48.550 those numbers we have to get other
00:14:53.140 00:14:53.150 equations and by putting some other
00:14:58.480 00:14:58.490 constants like the pressure drop then
00:15:01.360 00:15:01.370 the sock over all sides then we get
00:15:04.300 00:15:04.310 other equations and then we can try to
00:15:07.300 00:15:07.310 find out all this aah and AC so this is
00:15:12.790 00:15:12.800 the simplest situation when we have
00:15:15.750 00:15:15.760 assumed C R equals to 1 and we have
00:15:19.120 00:15:19.130 tried to design a simple tube in tube
00:15:23.230 00:15:23.240 heat exchanger now we may not expect
00:15:28.180 00:15:28.190 always that C H will be equal to the CC
00:15:33.280 00:15:33.290 or C R will be equals to 1 there may be
00:15:37.360 00:15:37.370 situation when CH is greater than C C or
00:15:41.740 00:15:41.750 it may also happen that CH is less than
00:15:46.090 00:15:46.100 C C that means C are either it will be
00:15:48.820 00:15:48.830 greater than 1 or it will be less than 1
00:15:52.080 00:15:52.090 in case C H is greater than C C we will
00:15:56.740 00:15:56.750 find that the temperature profile is
00:15:59.860 00:15:59.870 similar to the one like shown here for
00:16:04.480 00:16:04.490 the counter current heat exchanger when
00:16:08.020 00:16:08.030 CH is greater than C C we will find that
00:16:11.830 00:16:11.840 the cold fluid outlet temperature is
00:16:15.640 00:16:15.650 almost approaching the hot Inlet
00:16:20.470 00:16:20.480 temperature on the contrary if CH is
00:16:24.820 00:16:24.830 less than C C we will find that this hot
00:16:30.730 00:16:30.740 outlet is approaching the cold Inlet
00:16:36.220 00:16:36.230 temperature so the temperature profile
00:16:40.030 00:16:40.040 will look like this shown in this figure
00:16:43.600 00:16:43.610 so now let us consider for time being
00:16:47.170 00:16:47.180 that CH is greater than C C and let us
00:16:50.680 00:16:50.690 try to see
00:16:52.480 00:16:52.490 the or design problem for this situation
00:16:58.800 00:16:58.810 if we consider again a small elemental
00:17:02.530 00:17:02.540 length DL and then we can expect there
00:17:07.570 00:17:07.580 would be a small amount of heat DQ
00:17:10.630 00:17:10.640 getting transferred from the hot fluid
00:17:13.360 00:17:13.370 to the cold fluid through the separating
00:17:16.750 00:17:16.760 valve and all this assumptions which has
00:17:20.230 00:17:20.240 been made earlier except C R equals to
00:17:23.050 00:17:23.060 one all assumptions are still valid here
00:17:26.800 00:17:26.810 in this case also and only exception is
00:17:30.730 00:17:30.740 that we have assumed C H is greater than
00:17:33.220 00:17:33.230 C C now in this case what we will find
00:17:37.870 00:17:37.880 that the heat transfer coefficient or
00:17:40.390 00:17:40.400 the overall heat transfer between the
00:17:43.390 00:17:43.400 hot fluid to the cold fluid can be
00:17:46.030 00:17:46.040 related to the overall heat transfer
00:17:48.490 00:17:48.500 coefficient u and if we assume that the
00:17:53.080 00:17:53.090 area is distributed uniformly over the
00:17:55.870 00:17:55.880 entire length then a by L multiplied by
00:17:59.200 00:17:59.210 DL and th minus TC th is the hot site
00:18:04.980 00:18:04.990 temperature TC is the cold site
00:18:08.170 00:18:08.180 temperature at that point on in that
00:18:11.350 00:18:11.360 small elemental L length DL so now if we
00:18:15.640 00:18:15.650 make an energy balance for the hot fluid
00:18:19.720 00:18:19.730 we will find DK because 2 minus CH into
00:18:23.560 00:18:23.570 D th where D th is the change in
00:18:26.680 00:18:26.690 temperature within that small length DL
00:18:30.240 00:18:30.250 DQ is in terms of the cold fluid we can
00:18:36.220 00:18:36.230 write it that DQ is equal to minus CC d
00:18:40.270 00:18:40.280 TC where this DC DT C is the change in
00:18:44.830 00:18:44.840 temperature that is happening in the
00:18:48.250 00:18:48.260 small elemental length DL in the cold
00:18:52.390 00:18:52.400 fluid we can write this first equation
00:18:56.470 00:18:56.480 in this form where D H can be written as
00:18:59.950 00:18:59.960 DQ by CH with a negative sign and it is
00:19:03.910 00:19:03.920 C can be written as
00:19:06.190 00:19:06.200 - DQ by CC now let us try to write or
00:19:12.190 00:19:12.200 express D of th - DTC this is nothing
00:19:18.130 00:19:18.140 but the delta T over the length D DL so
00:19:23.380 00:19:23.390 d of delta T can now be expressed as
00:19:26.230 00:19:26.240 minus DQ if we take this one and this
00:19:29.289 00:19:29.299 expression I mean here in this equation
00:19:32.830 00:19:32.840 if we put we find that D th - DT C this
00:19:38.169 00:19:38.179 is we have taken from here this we have
00:19:40.779 00:19:40.789 taken from here and we are able to
00:19:44.169 00:19:44.179 express D of delta T is equals to minus
00:19:48.700 00:19:48.710 DQ into 1 by C H minus 1 by CC now we
00:19:58.450 00:19:58.460 can substitute this heat transfer from
00:20:04.299 00:20:04.309 here to this expression if we do that we
00:20:10.450 00:20:10.460 will find the equation is taking this
00:20:15.639 00:20:15.649 form what is that form d of d th d TC is
00:20:23.139 00:20:23.149 equals to u into a by LD l th minus TC
00:20:27.820 00:20:27.830 and 1 by CH - CC now what we are trying
00:20:31.960 00:20:31.970 we can now integrate it from this l
00:20:37.090 00:20:37.100 equals to 0 to l equals to l and when l
00:20:43.960 00:20:43.970 equals to 0 the corresponding difference
00:20:47.529 00:20:47.539 in temperature is delta T that is the
00:20:51.730 00:20:51.740 cost of delta T smaller one and this is
00:20:55.690 00:20:55.700 delta T larger one this is because we
00:21:00.669 00:21:00.679 have assumed t c h greater than CC so we
00:21:06.100 00:21:06.110 have the delta T is smaller on this side
00:21:09.250 00:21:09.260 and delta T large sorry this is delta T
00:21:12.970 00:21:12.980 L large on this side so if I integrate
00:21:18.760 00:21:18.770 it now over this
00:21:19.840 00:21:19.850 length what we will find is that log of
00:21:24.960 00:21:24.970 natural log of delta T large divided by
00:21:28.960 00:21:28.970 delta T small is equals to minus e way
00:21:31.779 00:21:31.789 into 1 by CH and minus 1 by CC now we
00:21:37.600 00:21:37.610 have this equation still remaining with
00:21:41.919 00:21:41.929 us cuba cost of CH into th n minus th
00:21:46.570 00:21:46.580 out that is the mass balance of the cold
00:21:49.720 00:21:49.730 fluid and this is the mass balance of
00:21:53.049 00:21:53.059 the study hot fluid and the cold fluid
00:21:55.630 00:21:55.640 this is for the hot fluid and this is
00:21:57.970 00:21:57.980 for the cold fluid this is known so if
00:22:00.909 00:22:00.919 we know this one we can take CH you know
00:22:05.890 00:22:05.900 this expression and put it here
00:22:08.950 00:22:08.960 we can take out CC and put this
00:22:13.330 00:22:13.340 expression in this one so if we do that
00:22:16.620 00:22:16.630 what you will find is an expression like
00:22:22.480 00:22:22.490 this we have replaced that one by CH
00:22:26.590 00:22:26.600 with this expression and 1 by CC with
00:22:30.580 00:22:30.590 this expression then with little algebra
00:22:36.010 00:22:36.020 if we do I mean we have rearranged with
00:22:38.830 00:22:38.840 this term we have taken th same as this
00:22:42.940 00:22:42.950 one we have taken you know this TC out
00:22:46.600 00:22:46.610 from there to here and this one is
00:22:50.529 00:22:50.539 somewhere here and this is like this
00:22:53.620 00:22:53.630 this is just to you know express this
00:22:57.159 00:22:57.169 temperature in terms of Delta TS and
00:23:00.580 00:23:00.590 Delta TL so the overall equation now
00:23:05.080 00:23:05.090 becomes Q equals to UA Delta TL minus
00:23:10.570 00:23:10.580 delta T s divided by natural log Delta
00:23:15.130 00:23:15.140 TL by delta T s so if we put this
00:23:20.320 00:23:20.330 expression as the natural log or sorry
00:23:25.750 00:23:25.760 the log mean temperature difference so
00:23:29.649 00:23:29.659 then it becomes Q because to UA delta T
00:23:32.950 00:23:32.960 LM or log mean so this is the log mean
00:23:37.810 00:23:37.820 temperature of this inter temperature
00:23:42.130 00:23:42.140 difference and then we can write the
00:23:47.470 00:23:47.480 heat transfer as this is the design
00:23:54.520 00:23:54.530 summary now what is known to us the Q
00:24:01.000 00:24:01.010 this is known because we know all the
00:24:03.670 00:24:03.680 exit temperatures now because this
00:24:07.480 00:24:07.490 exists and Paris is unknown we can also
00:24:10.120 00:24:10.130 find out this log mean temperature
00:24:13.000 00:24:13.010 difference this Q is known in this
00:24:16.480 00:24:16.490 equation the log mean temperature is
00:24:18.280 00:24:18.290 known so we can find out the overall
00:24:22.270 00:24:22.280 heat transfer coefficient which is
00:24:24.760 00:24:24.770 nothing but 1 by h HH plus 1 by h CAC so
00:24:32.200 00:24:32.210 again as we have discussed earlier once
00:24:35.830 00:24:35.840 we know this expression we can try to
00:24:38.860 00:24:38.870 find out the hot side and the cold side
00:24:43.620 00:24:43.630 parameters but this may be it may be
00:24:47.110 00:24:47.120 necessary that there will be certain
00:24:49.330 00:24:49.340 number of iterations now we have
00:24:55.200 00:24:55.210 discussed about this particular
00:24:58.270 00:24:58.280 situation
00:24:59.080 00:24:59.090 CH greater than CC and we have seen that
00:25:02.950 00:25:02.960 Q equals to you way into delta T of LM
00:25:11.560 00:25:11.570 now is it valid for CH less than C see
00:25:17.520 00:25:17.530 it can be shown that this is also valid
00:25:21.310 00:25:21.320 for this situation also only thing is
00:25:24.700 00:25:24.710 that this time that delta T large is
00:25:30.480 00:25:30.490 occurring on this side and delta T small
00:25:34.870 00:25:34.880 is occurring on this side in contrast to
00:25:37.960 00:25:37.970 this situation other things will remain
00:25:41.170 00:25:41.180 same the sign etc will also be taken
00:25:44.920 00:25:44.930 care accordingly
00:25:46.390 00:25:46.400 and the same expression also remains
00:25:49.270 00:25:49.280 valid for this situation now we want to
00:25:53.890 00:25:53.900 look for the counter current already
00:26:04.300 00:26:04.310 situation we have already looked for we
00:26:07.390 00:26:07.400 have already discussed now if we go for
00:26:10.150 00:26:10.160 a parallel flow heat exchanger or
00:26:12.130 00:26:12.140 co-current heat exchanger again by the
00:26:15.670 00:26:15.680 same way if we take a elemental length
00:26:18.220 00:26:18.230 over this heat exchangers length if we
00:26:22.720 00:26:22.730 take and small Delta L if we consider
00:26:25.990 00:26:26.000 and if we consider the temperature
00:26:27.670 00:26:27.680 difference if we write the energy
00:26:29.500 00:26:29.510 balance we will find that the heat
00:26:32.380 00:26:32.390 transfer overall heat transfer is given
00:26:35.200 00:26:35.210 by mu way into Delta TM this Delta TM in
00:26:39.340 00:26:39.350 this case we will have this as delta T
00:26:44.220 00:26:44.230 large and the difference on this side is
00:26:49.420 00:26:49.430 delta T small on this side other things
00:26:54.130 00:26:54.140 are remaining same so in a nutshell we
00:26:57.220 00:26:57.230 can see that all the counter current and
00:27:03.180 00:27:03.190 parallel flow or co-current heat
00:27:05.380 00:27:05.390 exchanger can be expressed by Q equals
00:27:10.840 00:27:10.850 to the heat transfer in this cases can
00:27:13.300 00:27:13.310 be expressed as Q equals to UA Delta TLM
00:27:17.310 00:27:17.320 in fact for all counter current parallel
00:27:23.170 00:27:23.180 flow as well as for situations where CR
00:27:27.400 00:27:27.410 equals to zero that is because two
00:27:29.200 00:27:29.210 condenser or RIBA I mean boiler
00:27:31.570 00:27:31.580 situations also we will find that this
00:27:34.720 00:27:34.730 relation remains valid now if we go to
00:27:39.940 00:27:39.950 the next light I mean if we find that
00:27:44.560 00:27:44.570 there is a cross flow heat exchanger do
00:27:48.160 00:27:48.170 we think that still we can use this
00:27:51.430 00:27:51.440 correlation we can use this correlation
00:27:54.250 00:27:54.260 I mean relation Q equals to UA Delta TLM
00:27:57.940 00:27:57.950 but with small
00:28:00.050 00:28:00.060 section factor because in this situation
00:28:03.050 00:28:03.060 this Delta TM or the mean temperature or
00:28:06.680 00:28:06.690 the log mean temperature that is not the
00:28:09.530 00:28:09.540 same in case of cross counter flow and
00:28:15.670 00:28:15.680 parallel flow heat exchanger if was
00:28:18.710 00:28:18.720 taken as 1 and if we put that relation
00:28:22.190 00:28:22.200 here we will find that this relation is
00:28:25.730 00:28:25.740 valid for the counter current and the
00:28:29.410 00:28:29.420 co-current heat exchanger but as we are
00:28:32.690 00:28:32.700 going to talk about a cross flow heat
00:28:34.940 00:28:34.950 exchanger we see that this will become
00:28:37.850 00:28:37.860 less than 1 so how to find out that
00:28:43.580 00:28:43.590 relation we will see that for different
00:28:52.240 00:28:52.250 heat exchanger configuration this has
00:28:56.000 00:28:56.010 already been calculated for our is and
00:28:59.680 00:28:59.690 this is related to the it is expressed
00:29:06.440 00:29:06.450 in terms of r and p two parameters which
00:29:11.000 00:29:11.010 are related to the two temperature
00:29:14.570 00:29:14.580 differences here this is T Inlet minus T
00:29:18.170 00:29:18.180 exit and this is the tube side that is T
00:29:23.060 00:29:23.070 0 minus TI this is one ratio the other
00:29:26.750 00:29:26.760 ratio is T 0 minus TI divided by the
00:29:31.220 00:29:31.230 maximum temperature difference that is T
00:29:33.500 00:29:33.510 I capital T I minus small T I this
00:29:36.920 00:29:36.930 expression has been taken from this
00:29:39.230 00:29:39.240 graph has been taken from AP entropy de
00:29:41.720 00:29:41.730 and David heat and mass transfer book so
00:29:49.240 00:29:49.250 similarly if the geometry is changing
00:29:55.540 00:29:55.550 from sailin tube this is multiple to
00:30:00.860 00:30:00.870 tube passes I mean it will be either two
00:30:05.390 00:30:05.400 tube or two tube multiples and there is
00:30:09.170 00:30:09.180 two shell side this is one cell side
00:30:12.170 00:30:12.180 another cell side
00:30:13.940 00:30:13.950 so this is the expression for now this
00:30:16.700 00:30:16.710 is the correction factor corresponding
00:30:18.409 00:30:18.419 to that configuration similarly the
00:30:27.620 00:30:27.630 other configurations will be like when
00:30:32.899 00:30:32.909 we have a cross flow heat exchanger with
00:30:36.169 00:30:36.179 single paths where both fluids are
00:30:38.180 00:30:38.190 unmixed or both fluids are mixed one
00:30:41.480 00:30:41.490 through it makes another fluid unmixed
00:30:43.490 00:30:43.500 this will correspond to a different
00:30:45.680 00:30:45.690 connection factor so based on this
00:30:48.200 00:30:48.210 values of the F factor we have to add
00:30:52.519 00:30:52.529 some correction to that ln TD method to
00:30:55.820 00:30:55.830 solve the Q equals to you way if Delta
00:30:59.990 00:31:00.000 TLM and then we can design the cross
00:31:03.500 00:31:03.510 flow heat exchanger thank you
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