Weight Limit
Adam Glatt
adam.g at sasktel.net
Mon Nov 11 12:59:27 AKST 2002
Won't equipping larger wings effectively decrease the tail moment and hurt stability?
----- Original Message -----
From: Buddy Brammer
To: discussion at nsrca.org
Sent: November 11, 2002 3:38 PM
Subject: Re: Weight Limit
Lance
I think my numbers went over most peoples head. None the less once they spend the time and money to build / design a competative pattern airplane they will come to the same conclusion that I have. wing loading not weight limit is the limiting factor and I believe that even if we removed the weight limit entirely pattern design would would not see radical changes with the 2 meter size limit we now have.
Buddy
>From: s.vannostrand at kodak.com
>Reply-To: discussion at nsrca.org
>To: discussion at nsrca.org
>Subject: Re: Weight Limit
>Date: Mon, 11 Nov 2002 12:38:06 -0600
>
>Buddy,
>I like opinions that are backed up with data and not just perceptions. My
>experience as a designer, like yours, leads me to the conclusion that
>there is a limit on how much airframe volume can exist in a 2m box and
>still have a precision aircraft. This limit may be larger than what we
>have today, but not much larger. A cubic airplane will not have the same
>stability as a monoplane or biplane. Also, a heavy plane with a bigger
>engine won't necessarily fly better either. As you state, there is a wing
>loading target that must be maintained.
> The cost of "exotic" materials in an airframe is not the expensive part.
> Too many people focus on this and forget where their money really goes.
>AeroSlave has carbon fiber planes for the same price or less than other
>manufacturers glass planes. I think the prices paid for carbon fiber
>exhaust systems have much more of a price premium than the premiums
>assessed on airplane kits. The emergence of digital servos has also upped
>the ante.
>
>Thanks for the numbers,
>--Lance
>
>===============================
>Ron and Georgie
>Good point! Except before any conclusions can be made reguarding weather
>raising the weight limit while keeping the 2 meter size will result in
>larger airplanes and increasing cost you must first study the limitations
>of a high performance pattern airplane.
>
>If you accept the fact a high performance pattern plane will have a wing
>loading of 100 sq. in. per pound then a 13 lb airplane will have a 1300
>sq. in. wing area . Lighter loading will result in less than acceptable
>fligh charesticts especially in higher wind conditions and I think that we
>will all agree that heavier wing loading will degrade performance.
>
>Adding a fatter and taller fuse and larger wings will certainly add
>weight.If you run the numbers this will be about a 15% increase in
>airframe weight for the 1300 sq. in. size.
>
>I personally think that increasing the airframe size/ weight 15% will have
>little effect on cost.
>
>Now if you increase size (Keeping the Maximum 2 meters limit ) you may
>need more power! and that will possibly result in engine design changes
>or the ability to adapt gasoline engines to pattern. If a gasoline engine
>can be used then it's a no brainer the cost of flying will be reduced .
>the more you fly with gas the more the average cost of pattern is lowered.
>If you fly 8 flights per gallon @ $16.00 per gallon the cost is $2.00 per
>flight. Gasoline @ $2.00 per gallon 25 cents per flight a savings of $1.75
>per flight. The savings there could reduce the cost of flying pattern by
>30%
>
>As a designer and builder of pattern airplanes given the current 2 meter
>limit I think the only reason for me to consider a larger design would be
>to cut my cost since I can find no other reason to go larger. If anyone
>has a valid reason speak up I am listening.
>
> And we have the age old argument that raising the limit will make
>many of the current near 2 meter size ARF's legal for pattern and bring
>more people into pattern at a reasonable cost. I think that may be true,
>and once they are hooked they will opt for a true pattern design.
>
>Buddy
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