"Ralph Jones" wrote in message
...
On Sat, 28 Apr 2007 21:32:47 -0600, "Wayne Paul"
wrote:

Bob,

Here is the reference:

http://mysite.verizon.net/engreenwel...teria_2004.pdf

You have it backward it is Weight / span ^ 2 0.62

In other words, it's the wing loading.

Ralph,

No, wing loading = weight / (span * MAC). Span loading does not consider
the wing's cord.

Wayne
HP-14 "6F"
http://www.soaridaho.com/Schreder
..