If I remember correctly, figures from Jeannette Rand, stated that each 6"
added to the wing length,
decreases the "G" load factor by 1/2 G. (please this my re-call and not
necessarily accurate).
This being true, and I increased my fuselage width by 4", and my center spar
by 6", does that add
2" to the actual wingth length or 6" ?
Ray Goree
raybeth...@sbcglobal.net
----- Original Message -----
From: "larry severson" <lar...@socal.rr.com>
To: "KRnet" <kr...@mylist.net>
Sent: Saturday, September 25, 2004 11:04 AM
Subject: Re: KR> G limit
> Physics is Physics.
>
> If a plane at a given weight will support a given G load, changing the
> weight changes the G load capability proportionately. The 100 lbs = 1 G is
> a nice, easy, safe way to calculate capability for planes in the
> weight/size of the KR2. The same ratio would work for the Q2.
>
> No, the plane's max G load does not drop that fast, but safe is better
> than
> sorry. It can be applied without the need for a calculator or any deep
> thought.
>
> Larry Severson
> Fountain Valley, CA 92708
> (714) 968-9852
> lar...@socal.rr.com
>
>
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