Mailing List lml@lancaironline.net Message #67236
From: Chris Zavatson <chris_zavatson@yahoo.com>
Sender: <marv@lancaironline.net>
Subject: [LML] Re: Lancair 320/360 performance and stability
Date: Tue, 01 Oct 2013 12:17:22 -0400
To: <lml@lancaironline.net>
Gary,
What is the flap chord length (center line of hinge to TE) at the root on a 235?  It must be shorter than a 320/360 given the 0.75" TE travel.
My trailing edge moves 1.48" to go from 0 to -7 degrees. 
An added complication is that the inboard edge of the flap is not perpendicular to the hinge.  If you measure along the inboard edge, you'll get a slightly longer measurement. 
Honestly, I prefer a direct angular measurement.  It takes all the geometry issues out of the equation.  I just checked the iPhone (Theodolite App) against my digital level.  The iPhone is a bit harder to read but it followed the level exactly.  The 'not free' version allows you to do screen captures.
 
Chris Zavatson
N91CZ
360std

From: Gary Edwards <gary21sn@hotmail.com>
To: lml@lancaironline.net
Sent: Tuesday, October 1, 2013 4:30 AM
Subject: [LML] Re: Lancair 320/360 performance and stability

Don't know if this is any help. 
 
The reflex position on the 235 airframe (same wing as the 320/360 wing) is up from the faired in with the fuselage position, which is 0 degrees.  -9 degrees is 0.75" (3/4") up from the fuselage.  So you could interpolate the distance to come up with the amount you are thinking of changing to.
 
Gary
LNC2
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