[NSRCA-discussion] Formula for figuring wing loading?
twtaylor
twtaylor at ftc-i.net
Tue Jul 25 12:16:43 AKDT 2006
Thanks Rick! Just what I was looking for.
_____
From: nsrca-discussion-bounces at lists.nsrca.org
[mailto:nsrca-discussion-bounces at lists.nsrca.org] On Behalf Of Rick Wallace
Sent: Tuesday, July 25, 2006 12:58 PM
To: nsrca-discussion at lists.nsrca.org
Subject: Re: [NSRCA-discussion] Formula for figuring wing loading?
Here's an excel spread sheet that should work for you.
Enter stuff in the yellow boxes:
wing area in sq in
model weight in lb and ounces
wing loading will calculate in the green boxes.
_____
From: "twtaylor" <twtaylor at ftc-i.net>
Reply-To: NSRCA Mailing List <nsrca-discussion at lists.nsrca.org>
To: <nsrca-discussion at lists.nsrca.org>
Subject: [NSRCA-discussion] Formula for figuring wing loading?
Date: Tue, 25 Jul 2006 10:36:20 -0400
For the mathematically impaired (me) Anyone know the formula? Id like to
plug and play some numbers. Thanks
>_______________________________________________
>NSRCA-discussion mailing list
>NSRCA-discussion at lists.nsrca.org
>http://lists.nsrca.org/mailman/listinfo/nsrca-discussion
-------------- next part --------------
An HTML attachment was scrubbed...
URL: http://lists.nsrca.org/pipermail/nsrca-discussion/attachments/20060725/6d2a4a9d/attachment.html
More information about the NSRCA-discussion
mailing list