Mailing List flyrotary@lancaironline.net Message #19802
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Re: [FlyRotary] Re: Cooling Inlet Areas/Bernie's RV9
Date: Tue, 5 Apr 2005 09:06:32 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
 I agree, Al.  
 
 I also made essential those points in my response the Rules of Thumb.
 
I would probably enlarge the intake area a bit from the current 28 sq inch to around 36 sq inches to take care of those Hot days.  I'll have to wait for that 95F day since last summer I spent waiting for prop and gearbox redo and did not get to test the intakes in the hottest months.  However, I have now flow with the reduced inlet for actually over two years and while temps to get elevated (200F on oil and 210F on coolant) on a high power climb, I find that acceptable given that my cruise temps are ideal between 170-180F.  I agree that prop wash and perhaps external diffusion plays a role as well.  Canards clearly have a different configuration to deal with.
 
Fuel flow actually shows greater that 180HP, but I like being a bit conservative in any claims in that area.  I have had fuel flow of 20 gph on a cold day and with that denser air.  Based on comparison with CAFE test (very credible) of  a fixed pitched prop 180HP Rv 6A  of the same weight my performance is at least as good in speed and  better in climb.  But again those are based on what I observe from my flight/engine instruments not what I would consider hard data.
 
The bottom line is I agree with Al, no one should get too carried away with my results.  I am experimenting and  pushing the limits because they only way you truly know where/what the limits are is to exceed them (hopefully by not too much).  As I have said several times I consider the 28 sq inches a minimum and I believe (correctly or not) that it works because the diffuser ducts are reasonably efficient and I do have a larger than "rule of thumb" out-let area. 
 
Perhaps Al, is correct and I am not producing 180 HP, but then I have a hard time understanding where my 120 lbs overweight RV gets its 1600-1800 fpm rate of climb otherwise.  But, I do agree with Al that what works for an engine producing 160HP may (will?) not  work for an engine producing 200HP.  If it does, then you have too much cooling capacity for the 160 HP installation and probably more cooling drag than necessary.
 
Also remember that if your installation is not exactly like the one you may be borrowing ideas from,  then yours is a different installation and the variable values may not be the same, the interaction and/or cumulative effect may not be the same, and therefore your results may not be the same.
 
Onward, get more of those rotaries flying!  Its getting tiresome seeing the same old rotary aircraft at Sun & Fun, need to have new blood show up.
 
Going out to fly and see what the newly tuned prop does before switching to manifold #6
 
 
Ed .
 
 
----- Original Message -----
From: Al Gietzen
Sent: Tuesday, April 05, 2005 1:02 AM
Subject: [FlyRotary] Re: Cooling Inlet Areas/Bernie's RV9

Before we get too carried away by Ed running with a lot less intake area than the ‘rule-of-thumb’ suggests; keep in mind that there are other variables, and there are some simple laws of physics.  The ‘rules of thumb’ assume ability for sustained high power with outside air temps of 90 – 100F.

 

It also assumes an air temp increase through the rad of 40-50F.  If you can achieve higher temp increase, then you can adjust down the flow.  The law of physics is that the air has a known specific heat; i.e., the amount of heat it will absorb per degree of heat up.  Knowing how much heat you have to dissipate, it tells you directly how much flow you need, and knowing how fast you are going tells you directly how big an opening you need to get that much air.  When the intakes are up front behind the prop you get some benefit from ‘external diffusion’ in front of the cowl, and perhaps some improved flow from the prop wash.

 

Having more outlet area then the 1.4 factor may also reduce require inlet area a bit, but at the expense of drag.  Ideally you would like to use some remaining pressure to accelerate the exit  air to near free stream velocity, the larger the outlet the slower the exit air, the more drag.

 

I would suggest that with 28 sq. in. of intake a.) Ed could not do sustained full power climb from low altitude on a 95F day, b.) he is getting greater than 50F air temp increase through the rads, and c.) he is actually generating less than 180 hp because fuel flow estimate will give you a max, which is not actually achieved in a rotary because of unburned fuel burning/going out the exhaust port.

 

I expect he may agree with a. and b. but never c. J; right Ed?

 

Clearly the ‘rules-of-thumb’ give you more inlet area than needed at cruise on an average day.  That’s why cowl flaps are good.

 

Al

 

> Al Gietzen wrote:

>

> > Doug;

> >

> > I agree with your ‘rule-of-thumb’ numbers. My analysis came up with

> > coolant inlet area in sq. in. of 1/3 the HP (.33) for climb out on a

> > 90F day. It assumes a 120kt climb speed for my Velocity. I used 45% of

> > that additional for the oil cooler. Assumes scoop efficiencies of 85%

> > or better.

> >

> > Al

> >

>

> > Second, even if cooling can get out, if it can't get in, it can't be

> > there to cool the heat exchangers. Rule of thumb: 0.3 sq. in. of

> > cowling inlet air opening per HP. 200 HP x .3 = 60 sq. in. Note: This

> > assumes a reasonably shaped inlet cowl which has been discussed online

> > often. IMHO: Berni's plane inlet shape and inlet cowl is fine, but I

> > question his inlet opening _area_.

> >

> snip

>

> > Don't mean to start another stream of threads on an old subject, but

> > we sweated over this one for 3 months and 3 systems and one might save

> > a lot of time by comparing ones system to these simple "works great"

> > rules of thumb which are the result of LOTS of technical and

> > experimental work.

> >

> > Doug Dempsey

> >

> > N6415Q and RV7 in process

> >

> > Colorado, USA

> >

>

> Don't won't do demean or dismiss your experimental work in any way, but

> Ed is running with half the inlet area, and unless something has changed

> with his new found power, he'd doing just fine. Just to be sure that

> we're all talking apples, I can confidently quote him at 28 in^2 inlet

> for coolant, which I believe is half of what you recommend above.

> Reality isn't meeting theory at eye level here, and everyone will be

> much better off if we know why.

>

> --

> This is by far the hardest lesson about freedom. It goes against

> instinct, and morality, to just sit back and watch people make

> mistakes. We want to help them, which means control them and their

> decisions, but in doing so we actually hurt them (and ourselves)."

>

 

I am running with 28 sq inches of total inlet area, much more outlet area

than Doug mentions and  not producing 200HP continuos.  My best estimate

based on fuel flow is I produce around 180HP perhaps a bit more on a cooler

morning.

 

 I agree apples and oranges get compared frequently.  But, rules of thumb

are just that - generally a place to get started.  I don't think anyone

would say that a rule of thumb means the "optimum" for a specific

installation.  Just good enough.  I have a rule of thumb that says given

enough surface area and airflow you WILL cool.  Not too helpful though and

certainly does not address the cooling drag you may impose.  I mean if your

rule of thumb says you have to have sufficient area to let the hot air out

and sufficient inlet to let the cold air in - well, OK, I can buy that - but

not too useful.  If you put numbers to it like Doug has done that becomes

more useful but is not the final answer.

 

For some of us, rules of thumb are simply a gore to understand what's behind

them. How did they come about, what do they mean?  To others they are a

heaven - sent- answer that does not require listening to or reading this

sort of stuff {:>).

 

So I am not certain we need to  necessarily even attempt to explain  Rules

of Thumb, they are simply a starting point that experience has shown will

work (most of the time).

 

Ed A

 

 

 

 

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