You meant "short span and long chord."  

--- On Mon, 12/19/11, Mark Goldman <bitshif...@gmail.com> wrote:

From: Mark Goldman <bitshif...@gmail.com>
Subject: RE: KR> A=L*W
To: "KRnet" <kr...@mylist.net>
List-Post: krnet@list.krnet.org
Date: Monday, December 19, 2011, 1:47 PM

On Dec 15, 2011 5:14 PM, "Barrett" <barret...@comcast.net> wrote:
<snip>
> Just thinking. A P-51 look-a-like would HAVE to have the radiator cooling
> duct under the fuse. So, what if that was turned into a pass-thru and the
> bottom was wing shaped for a bit of extra lift? (i.e.- flying fuselage)

I don't have my books on me right now, but everything I have read suggests
that short span and short chord lifting surfaces will end up costing more
in drag than they contribute in lift.  Aside from flying wing designs, I
don't believe there are any modern lifting body designs.  I can try to dig
up a reference tonight if you're interested.

-mdg
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