Sorry; Ed, your argument is bogus.
You changed horses in the middle of the stream, and that is not allowed.
You cannot suddenly change your assumed delta T, because that also requires
changing the inlet scoop, which changes the mass flow rate.
You size the inlet scoop to give you a
mass flow needed at a given delta T. If I expand that air to a large,
thin core, it’s velocity is slow, and I get the given delta T. If I
now expand the air half as much for a frontal area that is half as large and
the velocity is double, To get the same delta T (whatever that thickness is, probably double) I will get
a pressure drop about 4 times as high for the same delta T.
You have to compare them based on the same heat removal – same mass flow, same delta T
Al
-----Original Message-----
From: Rotary motors in aircraft
[mailto:flyrotary@lancaironline.net] On
Behalf Of Ed Anderson
Sent: Tuesday,
November 13, 2007 10:06 AM
To: Rotary motors in aircraft
Subject: [FlyRotary] Rebutal to
the rebutal {:>) Thick vs Thin was : Diffuser Configuration Comparison
Sure had me going for a spell,
however, I got out the equations and believe I can point out a different view
point.
If I understood you correctly, your
basic assertion is that the same mass flow is required for both thin and
thick radiators and since the thicker radiator has a smaller frontal
area it must therefore have a higher velocity air flow to generate the
same mass flow to remove the same heat. Furthermore the higher
velocity also translates into more drag (even with the reduced frontal area due
to the drag being proportional to the square of the velocity) - but all
the above is not necessarily
true.
In fact I found a NACA study
where they looked at the effects of using thicker radiators and I have worked
out the equations on a spreadsheet which I believe sheds some concrete facts on
the old thin Vs Thick debate - but, it is complex and I'll wait a bit before
springing it {:>).
However back to your
contention that both radiators the thin and the thick required the same mass
flow to remove the same amount of heat - it just isn't so and here is
why.
First, we have two radiators one is
1" thick and 1 square ft in frontal area, the second one is 1/2 square
feet of frontal area and twice (or more) as thick. Now turning to our
trusty equation for heat rejection and mass flow.
Q = m*Cp*DeltaT is the basic
equation that tells us how much heat we remove for a mass flow "m", a
specific heat (air = 0.24) and temperature increase in the medium (air) or
DeltaT.
Taking a specific example of say -
5000 Btu/min (which is about the amount of heat an NA 13B generates at 175 HP
that needs to be rejected by the coolant). We know the Cp so that leaves
the DeltaT and that is what makes the difference. We have to assume a
DeltaT, lets say 50F (yes, it could easily be different but bear with
me) then we have
m = 5000/(0.24)*(50)/60
= 6.94 lbm/sec of mass flow . and lets say we
have a 1 square foot radiator to get rid of that heat. Then the velocity
requires V1 = m/(p1A1) = 6.94 lbm/min/(.0765*1) = 90 ft/sec = 61.36 mph
through the 1 square foot radiator. Perhaps a bit higher than desirable
but that's what we get.
Now if I understood you
correctly your point is that the same mass flow is also required for
the smaller radiator (1/2 sq ft) to remove the same amount of heat and
therefore since frontal area is 1/2 the size, the velocity must be double
that of the larger radiator to get the same mass flow and remove the same
quantity of heat. But, it just isn't necessarily so.
Taking the same conditions as
before, except this time I use a DeltaT of 100F (hey! its permitted as I'm
using a different core here{:>) see further discussion on effects of
thickness on DeltaT). Now we have m = 5000/(0.24)*100/60 = 3.47 lbm/sec
of mass flow is required. That is 1/2 of the mass flow required with a
DeltaT of 50F.
Therefore even with 1/2 the frontal
area, I can use the same air velocity as before and remove the same amount of
heat with 1/2 the mass flow and with LESS drag because my frontal area is now
1/2 that of the thinner larger radiator and the velocity is the same. Now
you can say I cheated by having a different radiator, but that is certainly
what you would do - as that is what we are discussing are the relative merits
of thinner vs thicker for our application.
But, If you reduce the frontal
area of the radiator, then you must increase the thickness (or add more
fins, turbulators, etc) to increase its Heat transfer coefficient to
continue to reject sufficient heat to the air flow. Therefore, The
air temperature coming out of a thicker radiator is going to be higher than a
thin radiator. The reason is both radiators are flowing at the same
velocity (remember I did used the same velocity for both radiators),
and since the velocity of the flow is the same for both radiators, the air
spends more time (twice, three, four times depending on the thickness) in
the thicker core of the smaller radiator. The longer duration of the air in
the thicker core causes it to be absorb more heat and be raised to a higher
temperature than the thinner radiator, therefore the higher deltaT (for the
same velocity air).
This probably did not/and will not
convince you of the merits of the thicker vs thinner and besides I know your
reservations about my deductive reasoning {:>). So I am working on
understanding fully the Naca study I found that addresses the effect of
thickness on required mass flow and heat rejection. I believe it would be
considered a fairly credible source and will hopefully enable all to reach
their own conclusion. I think its going to blow the socks off this thick
vs thin debate - but, then I've been wrong before {:>)
Boy, this is fun!!! Sure keeps
the old brain working (hopefully).
Anyhow, Dave, I respectively
disagree with your assertion (see above) {:>)
----- Original Message -----
Sent: Tuesday, November 13, 2007
9:19 AM
Subject: [FlyRotary] Re: Thick vs
Thin was : Diffuser Configuration Comparison
> David Leonard wrote:
>> Why is it going slower? BECAUSE YOU HAVE DESIGNED YOUR THIN
RADIATOR SYSTEM
>> DUCTS SUCH THAT AN EQUAL AMOUNT OF AIR PASSES THROUGH AN EQUAL VOLUME
OF
>> RADIATOR AS WOULD OCCUR ON A THICK RADIATOR SYSTEM. (This is the
big if...
>> system design... but bear with me). ie, equal amount of air,
equal volume
>> of radiator - in the thin radiator system the air will be flowing more
>> slowly.
>>
>
> I agree with your concept, Dave, but I think you underestimate the
> difficulty of fitting a large faced radiator into the physical
> constraints of the area available in a small airplane. I worked on
> trying to use a large, 1" thick radiator for a while, and this was in
a
> delta planform. I had comparitively HUGE amounts of volume to work
> with. I eventually gave up, as there was just no reasonable way to
get
> a duct built around it that would slow the air down. As you increase
> the face area, you increase the size of the duct necessary to expand the
> air without separation. The best radiator and duct ever created will
be
> useless if we have to leave it on the ground because it doesn't fit in
> the airplane.
>
> I think the flow chart for sizing a radiator for our needs should follow
> something like this:
>
> 1) Mark out a space for the largest volume that you can fit a radiator
> and its associated ducting into. Insure that routing for the hoses
will
> be convenient, and the ducting can be made something resembling efficient.
>
> 2) Visit one of the websites like frigidair.com and find a radiator that
> meets the dimensional specs you came up with. Or contact Jerry and
have
> him make you one of that size.
>
> 3) If the core volume is less than 700 cubic inches, add another.
>
> 4) Go fly. If it is to cool (<160F), choke off the inlet a
little. If
> it is to hot (>200F), fiddle with the ducting.
>
> --
> Homepage: http://www.flyrotary.com/
> Archive and
UnSub: http://mail.lancaironline.net:81/lists/flyrotary/List.html