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11-20-2010, 10:17 AM
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Join Date: Dec 2006
Location: Arroyo Grande, CA
Posts: 938
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Smith's RV-6 wingtip tests
Jim has finally been able to make three sets of data runs at 4000', 6000', 8000' and 10,000' baro altitudes to compare with three sets of data he had taken previously with the standard tips. I took both data sets and obtained a second-order polynomial fit of each tip type vs density altitude. The results are presented below of the curve fit of TAS mph at 1000' intervals from a density altitude of 4000' to a density altitude of 12,000'.
dalt orig new
4000 189.9 197.0
5000 191.4 196.4
6000 192.0 195.6
7000 191.7 194.6
8000 190.4 193.4
9000 188.3 192.0
10,000 185.2 190.3
11,000 181.2 188.5
12,000 ----- 186.5
I didn't list the 12,000' value for the original tips as I felt that was at the extreme edge of the second-order curve and the closest three density altitudes with the original tips were 10,851, 10,885, and 10,998.
For those of a mathematical bent, the coefficients for the original tips are:
-4.669584E-7 * V^2 + 5.762168E-3 * V + 174.2846, and for the new tips:
-1.001908E-7 * V^2 + 2.854875E-4 * V + 197.5071
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11-20-2010, 10:37 AM
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Join Date: Oct 2009
Location: Victoria, BC, Canada
Posts: 3,926
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Which tips are these again? Do you have pictures? A 9mph increase at 4000' would be worth investigating for me... A lot of my flying around here is at or below 4000'.
__________________
Rob Prior
1996 RV-6 "Tweety" C-FRBP (formerly N196RV)
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11-20-2010, 11:01 AM
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Join Date: Sep 2006
Location: Douglas Flat, CA
Posts: 588
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The real question is, what do the short tips do to stall speeds and power-off glide ratios.
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11-20-2010, 11:44 AM
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Senior Curmudgeon
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Join Date: Sep 2005
Location: Dayton Airpark, NV A34
Posts: 15,408
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Well, maybe not "worthless" -----but photos sure would be nice
__________________
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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11-20-2010, 12:08 PM
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Join Date: Sep 2006
Location: Townsend, Montana
Posts: 3,179
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Post number 4 in the following thread, has a pic I believe
http://www.vansairforce.com/communit...ad.php?t=52556
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Retired Dam guy. Life is good.
Brian, N155BKsold but bought back.
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11-20-2010, 12:34 PM
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Join Date: Mar 2007
Location: Sonoma County
Posts: 3,821
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Quote:
Originally Posted by hydroguy2
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I like the looks of my stock flat top wing tips too much..... I don't know how much speed it would take for me to switch.
Let's just say........ ugly
How many G's would it take to tear one off?
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11-20-2010, 07:47 PM
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Join Date: May 2006
Location: Pocahontas MS
Posts: 3,884
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Hard to tell for sure from that one pic, but it looks like he should have a placard on the plane thanking Steve Whitman...
Charlie
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11-20-2010, 08:50 PM
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Join Date: Dec 2006
Location: Arroyo Grande, CA
Posts: 938
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Quote:
Originally Posted by Bob Kuykendall
The real question is, what do the short tips do to stall speeds and power-off glide ratios.
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These extended tips definitely lower takeoff, landing and stall speeds, while increasing rate-of-climb. Jim took a picture of a bunch of tufts near and at the tips just before a stall and they were straight back.
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11-20-2010, 09:28 PM
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Join Date: Aug 2005
Location: Atlanta, GA
Posts: 4,208
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Quote:
Originally Posted by elippse
These extended tips definitely lower takeoff, landing and stall speeds, while increasing rate-of-climb.
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RV-9 anyone?
__________________
Kyle Boatright
Marietta, GA
2001 RV-6 N46KB
2019(?) RV-10
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11-20-2010, 09:38 PM
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Join Date: Oct 2008
Location: Utah
Posts: 8,145
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Quote:
Originally Posted by Mike S
Well, maybe not "worthless" -----but photos sure would be nice
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I saw it at Oshkosh looks impressive.

Last edited by Vlad : 11-20-2010 at 10:35 PM.
Reason: added picture
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