This is true, you have to move the center aft to get more laminar flow.
Jeff vikensairfoil on the VK-30 had laminar flow back to 70% chord and it
would make the KR-1 more stable.
Sincerely
Jim
On Mon, 7 Nov 2005 14:56:59 -0000 (GMT) <pe...@heroic.co.uk> writes:
> Hi,
>
> How does the use of AS504* wings affect CG range.
>
> The wings having a different profile, presumably have a different
> centre
> of lift - my guess from looking at the profiles is that the centre
> of lift
> moves aft.
>
> So what is the impact on CG and is there a different practical CG
> range
> for aircraft with these wings?
>
>
>
>
>
> _______________________________________
> Search the KRnet Archives at
> http://www.maddyhome.com/krsrch/index.jsp
> to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
> please see other KRnet info at http://www.krnet.org/info.html
>
>
