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02-20-2010, 03:39 PM
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Join Date: Oct 2007
Location: Belvidere, IL
Posts: 169
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Jim Smith's tips:

__________________
David Shelton, Aerospace Engineer and Soaring Nut.
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02-20-2010, 04:19 PM
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Join Date: Feb 2007
Location: colorado
Posts: 873
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too ugly for my plane
Sorry Jim Smith, That is too ugly to be on an RV. Those tips and the spars and attachment weight surely has to offset any performance gain. Can you say double tapered wing?
Chris M
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02-21-2010, 01:57 AM
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Join Date: Mar 2005
Posts: 5,685
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Maybe tried later
Quote:
Originally Posted by elippse
...A flat tip with sharp edges top and bottom trips the flow around the tip from bottom to top and keeps the vortex near the tip. ...
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This would be fairly simple to implement with sheet metal, angle brackets and floating platenuts. I am thinking about it but not now - schedule crunch.
Bob Axsom
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02-21-2010, 08:06 AM
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Join Date: Jul 2005
Location: Detroit, MI
Posts: 1,587
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Easier yet?
Wouldn't it be easier to just attach with fixed platenuts inside the new, flat tips? I don't see what the angle brackets would do.
Quote:
Originally Posted by Bob Axsom
This would be fairly simple to implement with sheet metal, angle brackets and floating platenuts. I am thinking about it but not now - schedule crunch.
Bob Axsom
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__________________
H. Evan's RV-7A N17HH 240+ hours
"We can lift ourselves out of ignorance, we can find ourselves as creatures of excellence and intelligence and skill. We can be free! We can learn to fly!" -J.L. Seagull
Paid $25.00 "dues" net of PayPal cost for 2015, 2016, 2017 and 2018 (December).
This airplane is for sale: see website. my website
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02-21-2010, 11:37 AM
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Join Date: Dec 2006
Location: Arroyo Grande, CA
Posts: 938
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More on wingtips
Let me give you a few equations so you can play around with the numbers to see what performance increase you can see at different weights and density altitudes.
Parasite drag, lb., = Q X AP; Induced drag = W^2/ Q X S^2 X PI X e, where:
Q=rho X V^2 / 2, AP=equivalent parasite drag area, sq. ft. W=weight, lb., S=span, ft., PI=3.1416, e=Oswald efficiency factor, V=TAS,mph X 22/15, rho=.00237689(1-6.88E-6 X dalt)^4.256.
Add the two drags, multiply by V, and divide by 550. That will give you the total drag power required.
Now let me show you the resulting HP required from increasing the span by 13% to 26' and reducing the area by 13% to 97 sq. ft., using 200 mph TAS at 1400 lb and 1600 lb at three different density altitudes. It also shows the HP difference and the speed increase that could be seen.
1400 lb 1600 lb
dalt 23/110 26/97 23/110 29/97
1000' 130.7 124.9 4.7% 203.1 133.1 126.7 5.0% 203.3
7500' 110.5 105.0 5.2% 203.4 113.4 107.3 5.7% 203.7
14,000' 93.9 88.6 6.0% 203.9 97.5 91.4 6.7% 204.3
You can use these values to check your own calculations and a spreadsheet program to see if you've set it up right.
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02-21-2010, 12:24 PM
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Join Date: Mar 2005
Posts: 5,685
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Not Really
Quote:
Originally Posted by hevansrv7a
Wouldn't it be easier to just attach with fixed platenuts inside the new, flat tips? I don't see what the angle brackets would do.
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The old semi-flat tips with the rounded edges are considered offerings to the God of Speed - N_G. If I do this I will start with a flat 0.016" aluminum tip plate butted right up against the end of the wing skin. The angle brackets will be riveted to the inside of the tip plates and will extend inside the wing skin aligned with the existing tip mounting holes. The floating platenuts will be riveted to the angle brackets and pick up the #8 flathead tip mounting screws. After I have the 3/32" platenut mounting holes drilled in the angle brackets using a non-floating platenut as a drill guide I will open the center hole to 3/8" to clear the wing skin dimples. I hope that clarifies the approach. I may start with an oversized tip plate (anyone remember Ron St Jean's Ram Rod 750?) then test and trim and test and trim ... until the edge of the tip plate conforms exactly to the size of the end of the wing.
Bob Axsom
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02-21-2010, 02:02 PM
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Join Date: Dec 2006
Location: Arroyo Grande, CA
Posts: 938
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[quote=Christopher Murphy;407451]Sorry Jim Smith, That is too ugly to be on an RV.Chris M
Chris; you forgot to write IMHO! You probably wouldn't like the triangular extensions on my Lancair, or those on the Diamond Katana and the latest Boeing jets.
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02-21-2010, 04:08 PM
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Join Date: Dec 2008
Location: Ontario, Canada
Posts: 464
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Quote:
Originally Posted by Bob Axsom
If I do this I will start with a flat 0.016" aluminum tip plate butted right up against the end of the wing skin. The angle brackets will be riveted to the inside of the tip plates and will extend inside the wing skin aligned with the existing tip mounting holes.
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Bob,
did you guys get that space camera going on my hanger? I was sure the lead sheild would prevent it !!
You are thinking what i have started to do. quick and easy and no fibreglass.
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02-21-2010, 05:21 PM
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Join Date: Feb 2007
Location: colorado
Posts: 873
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its just a matter of taste
[quote=elippse;407657]
Quote:
Originally Posted by Christopher Murphy
Sorry Jim Smith, That is too ugly to be on an RV.Chris M
Chris; you forgot to write IMHO! You probably wouldn't like the triangular extensions on my Lancair, or those on the Diamond Katana and the latest Boeing jets.
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To each his own I guess.. I was just being sarcastic. The legacy's wing doesn't look bad and I don't know about the Diamond. I am pretty familiar with the Boeing planes and I don't recall seeing anything like that on a Boeing.
I saw a 4 blade prop somewhere that had that type of tip on it. It was pretty ugly too....IMHO.
Chris M
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02-21-2010, 06:22 PM
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Senior Curmudgeon
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Join Date: Sep 2005
Location: Dayton Airpark, NV A34
Posts: 15,430
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Quote:
Originally Posted by Christopher Murphy
I saw a 4 blade prop somewhere that had that type of tip on it. It was pretty ugly too....IMHO.
Chris M
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I saw that prop too, on a race plane at Reno-------kicked but t on the rest of the field big time----like 30 mph IIRC
__________________
Mike Starkey
VAF 909
Rv-10, N210LM.
Flying as of 12/4/2010
Phase 1 done, 2/4/2011 
Sold after 240+ wonderful hours of flight.
"Flying the airplane is more important than radioing your plight to a person on the ground incapable of understanding or doing anything about it."
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