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ashralf
Joined: 24 Sep 2007
Posts: 1
Location: malaysia
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 Posted: Mon Sep 24, 2007 8:16 pm Post subject: stol ch701 wing profile |
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i would like to ask for stol ch701 wing profile
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ch701builder
Joined: 07 Feb 2006
Posts: 119
Location: N38.9947,W105.1305,ALT. 9,100'
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| Posted: Mon Sep 24, 2007 8:39 pm Post subject: stol ch701 wing profile |
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The airfoil is a NACA 6515 mod.
http://www.ae.uiuc.edu/m-selig/ads/aircraft.html
Search for Heintz. I am figuring that most of these are correct.
Keith
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xl(at)prosody.org
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| Posted: Mon Sep 24, 2007 9:49 pm Post subject: stol ch701 wing profile |
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Wow, that's a neat resource!
The CH601XL has the same wing root airfoil as a
Lockheed 1049 Constellation and a King Air.
Next time one of those passes me I'll feel smarter.
A King Air passed about 500 feet directly over me
Sunday over Seattle - same wing root profile, neat.
Joe E (at) BFI
CH601XL, 491 hours
Jabiru 3300, Sensenich wood prop 49x64
On Mon, 24 Sep 2007, Ashcraft, Keith -AES wrote:
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John Bolding
Joined: 23 May 2006
Posts: 281
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| Posted: Tue Sep 25, 2007 6:16 am Post subject: stol ch701 wing profile |
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The airfoil is the 65018 18% thick. I assume you are asking about the airfoil in total,
slat and all. It isn't exactly a 65018 either as Chris made construction a little easier for us by eliminating the slight undercamber on the lower surface and he flattened the top a little in the spar area so we could use angle extrusions for spar caps.
LOW&SLO
John Bolding
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