<html xmlns:v="urn:schemas-microsoft-com:vml" xmlns:o="urn:schemas-microsoft-com:office:office" xmlns:w="urn:schemas-microsoft-com:office:word" xmlns:st1="urn:schemas-microsoft-com:office:smarttags" xmlns="http://www.w3.org/TR/REC-html40">
<head>
<meta http-equiv=Content-Type content="text/html; charset=us-ascii">
<meta name=Generator content="Microsoft Word 11 (filtered medium)">
<!--[if !mso]>
<style>
v\:* {behavior:url(#default#VML);}
o\:* {behavior:url(#default#VML);}
w\:* {behavior:url(#default#VML);}
.shape {behavior:url(#default#VML);}
</style>
<![endif]--><o:SmartTagType
namespaceuri="urn:schemas-microsoft-com:office:smarttags" name="PersonName"/>
<!--[if !mso]>
<style>
st1\:*{behavior:url(#default#ieooui) }
</style>
<![endif]-->
<style>
<!--
/* Font Definitions */
@font-face
{font-family:Tahoma;
panose-1:2 11 6 4 3 5 4 4 2 4;}
/* Style Definitions */
p.MsoNormal, li.MsoNormal, div.MsoNormal
{margin:0in;
margin-bottom:.0001pt;
font-size:12.0pt;
font-family:"Times New Roman";}
a:link, span.MsoHyperlink
{color:blue;
text-decoration:underline;}
a:visited, span.MsoHyperlinkFollowed
{color:purple;
text-decoration:underline;}
p
{mso-margin-top-alt:auto;
margin-right:0in;
mso-margin-bottom-alt:auto;
margin-left:0in;
font-size:12.0pt;
font-family:"Times New Roman";}
span.emailstyle17
{font-family:Arial;
color:windowtext;}
span.EmailStyle19
{mso-style-type:personal-reply;
font-family:Arial;
color:navy;}
@page Section1
{size:8.5in 11.0in;
margin:1.0in 1.25in 1.0in 1.25in;}
div.Section1
{page:Section1;}
-->
</style>
</head>
<body lang=EN-US link=blue vlink=purple>
<div class=Section1>
<p class=MsoNormal><font size=2 color=navy face=Arial><span style='font-size:
10.0pt;font-family:Arial;color:navy'>Thanks Rick! Just what I was looking for.<o:p></o:p></span></font></p>
<p class=MsoNormal><font size=2 color=navy face=Arial><span style='font-size:
10.0pt;font-family:Arial;color:navy'><o:p> </o:p></span></font></p>
<div>
<div class=MsoNormal align=center style='text-align:center'><font size=3
face="Times New Roman"><span style='font-size:12.0pt'>
<hr size=2 width="100%" align=center tabindex=-1>
</span></font></div>
<p class=MsoNormal><b><font size=2 face=Tahoma><span style='font-size:10.0pt;
font-family:Tahoma;font-weight:bold'>From:</span></font></b><font size=2
face=Tahoma><span style='font-size:10.0pt;font-family:Tahoma'>
nsrca-discussion-bounces@lists.nsrca.org [mailto:nsrca-discussion-bounces@lists.nsrca.org]
<b><span style='font-weight:bold'>On Behalf Of </span></b>Rick Wallace<br>
<b><span style='font-weight:bold'>Sent:</span></b> Tuesday, July 25, 2006 12:58
PM<br>
<b><span style='font-weight:bold'>To:</span></b> <st1:PersonName w:st="on">nsrca-discussion@lists.nsrca.org</st1:PersonName><br>
<b><span style='font-weight:bold'>Subject:</span></b> Re: [NSRCA-discussion]
Formula for figuring wing loading?</span></font><o:p></o:p></p>
</div>
<p class=MsoNormal><font size=3 face="Times New Roman"><span style='font-size:
12.0pt'><o:p> </o:p></span></font></p>
<div>
<p><font size=3 face="Times New Roman"><span style='font-size:12.0pt'>Here's an
excel spread sheet that should work for you. <o:p></o:p></span></font></p>
<p><font size=3 face="Times New Roman"><span style='font-size:12.0pt'>Enter
stuff in the yellow boxes: <br>
wing area in sq in<br>
model weight in lb and ounces <o:p></o:p></span></font></p>
<p><font size=3 face="Times New Roman"><span style='font-size:12.0pt'>wing
loading will calculate in the green boxes. <o:p></o:p></span></font></p>
<div class=MsoNormal align=center style='text-align:center'><font size=1
face=Tahoma><span style='font-size:8.5pt;font-family:Tahoma'>
<hr size=1 width="100%" noshade color="#a0c6e5" align=center>
</span></font></div>
<p class=MsoNormal style='margin-bottom:12.0pt'><font size=1 face=Tahoma><span
style='font-size:8.5pt;font-family:Tahoma'>From: <i><span style='font-style:
italic'>"twtaylor" <twtaylor@ftc-i.net></span></i><br>
Reply-To: <i><span style='font-style:italic'>NSRCA Mailing List <<st1:PersonName
w:st="on">nsrca-discussion@lists.nsrca.org</st1:PersonName>></span></i><br>
To: <i><span style='font-style:italic'><<st1:PersonName w:st="on">nsrca-discussion@lists.nsrca.org</st1:PersonName>></span></i><br>
Subject: <i><span style='font-style:italic'>[NSRCA-discussion] Formula for
figuring wing loading?</span></i><br>
Date: <i><span style='font-style:italic'>Tue, 25 Jul 2006 10:36:20 -0400</span></i><o:p></o:p></span></font></p>
<blockquote style='border:none;border-left:solid #A0C6E5 1.5pt;padding:0in 0in 0in 4.0pt;
margin-left:3.75pt;margin-top:5.0pt;margin-right:0in;margin-bottom:5.0pt'>
<p class=MsoNormal><font size=2 face=Arial><span style='font-size:10.0pt;
font-family:Arial'>For the mathematically impaired (me) Anyone know the
formula? Id like to plug and play some numbers. Thanks</span></font><o:p></o:p></p>
<p class=MsoNormal><font size=1 face=Tahoma><span style='font-size:8.5pt;
font-family:Tahoma'><o:p> </o:p></span></font></p>
<p><font size=1 face=Tahoma><span style='font-size:8.5pt;font-family:Tahoma'>>_______________________________________________<br>
>NSRCA-discussion mailing list<br>
>NSRCA-discussion@lists.nsrca.org<br>
>http://lists.nsrca.org/mailman/listinfo/nsrca-discussion<o:p></o:p></span></font></p>
</blockquote>
</div>
</div>
</body>
</html>