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Spitfire - Efficiency of Cooling and Thrust

05/25/2010 5:36 AM

The weekend just gone by had a programme on the goggle box about the Supermarine Spitfire. It was quite interesting until the presenter started to explain about the cooling system.

He said that the radiator inlet below the wing was very efficient for cooling the engine and the added bonus was that the compressed air when exhausted, came out faster than tyhe air going in, providing some thrust.

At that point a few expletives were thrown at the TV and the dumbing down of so called educational TV.

I immediately dismissed his comment and was thinking about the conservation of energy, efficiency problems etc.

But when I thought about it a bit longer. There is actually energy being passed to the air from the cooling system of the plane.

My question/discussion point is how much could this effect the efficiency of the air going into the cooling box and being ejected out.

How much energy(Drag) is lost from the plane due to the air being dragged into the box and how much could an increase in the energy from the heat improve this system. Is the heat going into the air not doing anything or is it as the presenter "Informed" me actually providing a small bit of thrust?

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#1

Re: Spitfire cooling and thrust

05/25/2010 5:49 AM

I think you know the answer, but, just like me are too lazy/dissinclined to do the arithmetic!
Or to put it another way, I don't s'pose the trust is any more than the drag.
I would imagine the the thing was designed empirically anyway, start with a reasoanble sized rad and make it smaller and smaller until you get overheating and then go back a bit. I don't s'pose that thrust thing was ever even considered.
I agree there is some wince making 'science' on TV, but maybe some is better than none? Please no more Richard 'look at me being a cute schoolboy with flopsy hair with one fixed mode of presenting' Hammond...it was only amusing the first 'n' times.
Del

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#2
In reply to #1

Re: Spitfire cooling and thrust

05/25/2010 5:56 AM

It was Rimmer from Red Dwarf.

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#3
In reply to #2

Re: Spitfire cooling and thrust

05/25/2010 6:28 AM

Oh well... I'd rather the little cutie from scrapheap challenge.
Del

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#4

Re: Spitfire - Efficiency of Cooling and Thrust

05/25/2010 9:27 AM

The added heat will provide a minuscule amount of additional thrust. How much?

I don't know.

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#5

Re: Spitfire - Efficiency of Cooling and Thrust

05/25/2010 10:31 PM

This is the ramjet effect. The air is heated and expands as a result, giving a higher pressure and/or velocity of air at the exit. Direct conversion of heat energy into thrust. It was apparently quite effective on the P51, - a later design - although I do not know the numbers.

Ramjet efficiency goes up rapidly with speed. It starts becoming usable at about 400 mph and gets much more efficient at Mach 1 and faster. The SR-71 is basically a ramjet driven airplane above Mach 1. The new SCRAMJETs take this the next step above Mach 3.

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#12
In reply to #5

Re: Spitfire - Efficiency of Cooling and Thrust

05/26/2010 10:44 AM

In a ramjet or scramjet, fuel is added and combusted, providing LARGE amounts of heat. Here the only heat added is from the radiator. No comparison!

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#6

Re: Spitfire - Efficiency of Cooling and Thrust

05/25/2010 11:43 PM

This is commonly quoted as a net thrust (for these water cooled aircraft) and I don't see any reason why it would not be so with sensible design.

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#7
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Re: Spitfire - Efficiency of Cooling and Thrust

05/26/2010 2:24 AM

I don't see any reason why it would not be so with sensible design.

Hmmm, maybe because most of the energy from the expansion of the combustion has already been used to move pistons up and down and all that remains is some low grade waste heat which isn't at pressure (remember this isn't even waste exhaust gas, it's the cooling air).
OK you car isn't quite the same as an Spitfire, but how much spare energy is there in the hot water in the radiator...maybe enough for a fry up or a cup of tea?
Agreed ow't is better than now't and with a Messershmitt chasing you, then anything helps, but I would venture to suggest that the aerodynamics of the plane and the air intake were more significant than the resultant thrust of warming air up by 100degrees or so, I mean, it's not being turned to steam!
Del

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#8
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Re: Spitfire - Efficiency of Cooling and Thrust

05/26/2010 2:46 AM

The thermodynamic efficiency of a well designed gasoline engine is about 20-25%. So you are dumping a lot of heat into this oil cooler at about 180 F, at least three times what you are getting out to the prop. The thermodynamic efficiency of heat to thrust may be low, but it was enough to specifically design the P-51 cooling system to use it. A moderate amount of extra thrust at 400 mph amounts to a lot of power.

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#9
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Re: Spitfire - Efficiency of Cooling and Thrust

05/26/2010 3:02 AM

A moderate amount of extra thrust at 400 mph amounts to a lot of power.
What??? That statement doesn't stand up to careful examination.

A 'moderate amount' of extra power results in little extra velocity when drag is proportional to the cube of velocity.

Del
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#13
In reply to #9

Re: Spitfire - Efficiency of Cooling and Thrust

05/26/2010 8:29 PM

"A moderate amount of extra thrust at 400 mph amounts to a lot of power. What??? That statement doesn't stand up to careful examination.

A 'moderate amount' of extra power results in little extra velocity when drag is proportional to the cube of velocity."

You're looking at it backwards. Power equals thrust times velocity, so one extra pound of thrust at 400 mph is 1 lb * 400*1.5 ft/s = 600 lb*ft/s, a little over one horsepower for each pound of additional thrust. Bear in mind this is net, delivered horsepower - equivalent to at least five thermal horsepower of fuel consumption if it had been generated by putting in a bigger engine.

This is why engineers of the Thirties and Forties were so eager to derive extra thrust from engine exhaust - with or without augmentors - and from coolant heat. It also motivated efforts to use exhaust flow to pump cooling air.

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#14
In reply to #13

Re: Spitfire - Efficiency of Cooling and Thrust

05/27/2010 3:04 AM

ArrrrHHHGGGG.
Jeez... NO... I'm not looking at it backwards!
That's exactly the point I was making (obviously, far too subtely)!
He'd missused his terms!

The point I was making is that it WON'T produce a 'moderate amount of THRUST.
It WILL produce a moderate amount of POWER.

You are in fact agreeing with me! (I'd alread marked your answer as 'Good')
(Not to self type slowly and in block caps so people will understand cat language)
Del
(And the doc wonders why I have high blood pressure... clam calm)

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#15
In reply to #14

Re: Spitfire - Efficiency of Cooling and Thrust

05/27/2010 1:00 PM

"ArrrrHHHGGGG.


Jeez... NO... I'm not looking at it backwards!
That's exactly the point I was making (obviously, far too subtely)!

He'd missused his terms!"

Ooops.

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#10

Re: Spitfire - Efficiency of Cooling and Thrust

05/26/2010 3:40 AM

I think if we are to reach a sensible conclusion it needs someone to put some figures to it. If they show a useful amount of power I'll happily grovel and distribute cases of KrisDelTM virtual beer to all concerned.
Del

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#11

Re: Spitfire - Efficiency of Cooling and Thrust

05/26/2010 5:20 AM

"He said that the radiator inlet below the wing was very efficient for cooling the engine and the added bonus was that the compressed air when exhausted, came out faster than tyhe air going in, providing some thrust."

The so-called "Meredith Effect" was studied in Britain starting in the 1930s, so it is nearly certain that it was considered in the design of the Spitfire cooling shroud. It was certainly a consideration in designing the P-51 belly shroud. How much thrust is possible depends on your assumptions, and it must be quite low in any case because of the low thermal efficiency of thermal ducts at low speeds (low pressure ratios). But whether you believe in net thrust or not, at the very least designing with this in mind will reduce cooling drag. This is still a very relevant topic, because the cooling drag of piston-engined aircraft is generally several times what theory says it must be, per Bruce Carmichael.

Original Meredith paper: Note On The Cooling Of Aircraft Engines With Special Reference To Ethylene Glycol Radiators Enclosed In Ducts by F. W. Meredith, B.A. ARC Reports and Memoranda No. 1683. Available here: http://aerade.cranfield.ac.uk/results.php?Simplequery=1683&sf=RN&st=OR&rs=ARC

Another interesting paper is Rauscher & Phillips: Propulsive Effect of Radiator and Exhaust Ducting (Journal of the Aeronautical Sciences, 1941). Available from research libraries and from my catalog at http://www.archivale.com/catalog .

Bruce Carmichael's discussion of cooling drag is in his book Personal Aircraft Drag Reduction. It's reviewed on my blog at http://archivale.com/weblog/?p=102 . The review includes ordering instructions in case you get hooked.

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