[NSRCA-discussion] Gas vs Alcohol (was Newslist is flawed)

Bill Glaze billglaze at bellsouth.net
Mon Dec 14 13:26:00 AKST 2009


Assuredly, it's not a direct trade-off; Stochiometric is different for the different fuels, of course.  And the fact remains that running pure methanol will provide approximately 15% more horsepower for the fuel burned, which, again, is about twice that required for gasoline.  What it amounts to is that gasoline is the most efficient of the three substances, but, in our case, I will admit readily that efficiency is far down the list of requirements.  I have been running some tests, (of which the sampling is small, admittedly) and I was surprised at the small rpm difference between 15% standard Morgan Cool Power, and 30% Heli.  If you need, or can discern, the small difference involved, then of course it justifies the use of the 30% stuff.  In my case, it doesn't seem to justify the usage.  When one mixes in the Latent Heat of Vaporization, the waters are muddied even more, but it probably is of small concern in engines the size of ours, due to the small swept volume, and the variation of conditions having to do with cooling, both external and internal.
Bill Glaze
  ----- Original Message ----- 
  From: Bob Richards 
  To: General pattern discussion 
  Sent: Monday, December 14, 2009 5:08 PM
  Subject: Re: [NSRCA-discussion] Gas vs Alcohol (was Newslist is flawed)


        Bill,

        The heat energy per unit has little to do with the power we get from an internal combustion engine. The limiting factor is how much air we can get into the engine. Each fuel has an optimum ratio to be mixed with the amount of air that enters the engine. Gasoline burns the leanest. Methanol burns much richer, so more fuel goes into the engine per stroke. Nitro is even richer.  

        I've also read that nitro expands to a much larger volume when it burns, even though it puts out less heat per unit than methanol, which is one reason why nitro by itself puts out much more power than methanol. I may open a can of worms when I say this, but it has been my experience in both pattern planes and helicopters that higher nitro makes the engine run cooler. 

        Think about it, methanol puts out less heat per unit, but develops more power than gasoline. Gasoline engines must have larger cooling fins, even though less power is being developed. Gasoline burns so lean compared to methanol, this is the reason why gasoline carbs are more complicated than alcohol carbs. Add nitro, then the needle must be opened more and becomes less sensitive. This may be an over-simplistic explanation because the thermodynamics are vastly different (methanol provides a lot of internal cooling as it atomizes) but it works for me. :-)

        Bob R.




        --- On Mon, 12/14/09, Bill Glaze <billglaze at bellsouth.net> wrote:


          From: Bill Glaze <billglaze at bellsouth.net>
          Subject: Re: [NSRCA-discussion] This email list is flawed in my opinion.
          To: "General pattern discussion" <nsrca-discussion at lists.nsrca.org>
          Date: Monday, December 14, 2009, 6:28 PM


           
          The specific heat generated by gasoline is about twice the specific heat generated by alcohol, which, in turn is about twice the specific heat generated by nitro.  In other words, on a mass basis, nitro is a more inefficient fuel on a pure basis than alcohol, which is less efficient than gasoline. (from a volume/efficiency standpoint)
          Or so my handbook stated when I was building competition engines.  Then why use nitro at all?  Well, because it generates more O2 than it needs to burn, thereby helping the other "combustibles" complete their combustion, and it's possible to run a hellacious load of nitro per cycle because of it's burn characteristics.
          Bill Glaze
            ----- Original Message ----- 
            From: Vicente "Vince" Bortone 
            To: General pattern discussion 
            Sent: Sunday, December 13, 2009 8:48 AM
            Subject: Re: [NSRCA-discussion] This email list is flawed in my opinion.


            Matt,

            It will be very interesting to see your results.  I had the chance to build and fly the Abbra with ZDZ 40.  I was able to comparare the same plane with OS160 back-to-back.  Clearly the ZDZ 40 was behind in power (or power-to-weight ratio) when compared with the OS 160 when doing the Master schedule of that time.  I am sure that less fuel consumption with less BTU content means less power.  The Abbra with the ZDZ 40 was ~3-4 oz over 11 lbs.  The OS 160 Abbra was 9.8 lbs.  I am not sure now what the new gasoline engines manufactures are doing to increase the power.  I believe that an improvement in the design of gas engines is required to make it usable for pattern. 

            Vicente "Vince" Bortone

            ----- Original Message -----
            From: rcmaster199 at aol.com
            To: nsrca-discussion at lists.nsrca.org
            Sent: Saturday, December 12, 2009 10:46:09 PM GMT -06:00 US/Canada Central
            Subject: Re: [NSRCA-discussion] This email list is flawed in my opinion.


            Yes that's true. When I was mixing my fuel I needed to do it by volume until I figgered what the volume weighed for each of the nitro blends I was mixing..... 30% nitro is around 10% denser (weighs around 10% more for a tankful) than 15% nitro. 

            Soooo....the guys who are running the YS not only use much larger tanks but their tanks weigh more when full than they would have running lower nitro. But YS is a dawg on lower nitro. You gotta admire YS Marketing strategy

            Yet another reason I am looking into gasoline powerplants for pattern. Gas is significantly less dense than 30% nitro blend and gas engines demand less fuel to begin with. A 320 cc tank (around 11 ozs) will run the 30 cc engine for around 12 minutes, enough for about 1 2/3 master schedules.



            MattK





            -----Original Message-----
            From: Verne Koester <verne at twmi.rr.com>
            To: 'General pattern discussion' <nsrca-discussion at lists.nsrca.org>
            Sent: Sat, Dec 12, 2009 11:24 pm
            Subject: Re: [NSRCA-discussion] This email list is flawed in my opinion.


            The weight of fuel is going to depend in large part on the percentage of nitro. Nitro is the heaviest component. Don’t believe it? Go to the hobby shop and pick up a gallon of 5% with one hand and 30% with the other, preferably from the same manufacturer. You’ll be surprised. I know I was when a fuel manufacturer showed me at Toledo about twenty years ago. Fortunately, pilots with glow planes are weighed without the fuel so they don’t have to worry about that…

            Verne

            From: nsrca-discussion-bounces at lists.nsrca.org [mailto:nsrca-discussion-bounces at lists.nsrca.org] On Behalf Of Bill's Email
            Sent: Saturday, December 12, 2009 8:16 PM
            To: General pattern discussion
            Subject: Re: [NSRCA-discussion] This email list is flawed in my opinion.

            Ed Alt wrote: 
            About 0.75 oz per fluid oz.


            I just weighed a gallon of fuel I have here. It was 7.8 pounds including the plastic jig. 0.75 ounces per fluid ounce would mean the jug weighs +/- 29 ounces (1.8 pounds). 
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