Mailing List flyrotary@lancaironline.net Message #8527
From: Finn Lassen <finn.lassen@verizon.net>
Subject: Re: [FlyRotary] Trim Adjustment was Re: [FlyRotary] Re: engine mount geometry
Date: Sun, 23 May 2004 14:30:17 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Ed Anderson wrote:
Message
I think this gets to be a bit of a complex aerodynamic Question.  Rudder or any trim offers some drag, however if it aligns the body of the aircraft more with the airstream, there could be an overall reduction in drag.  I would hesitate to offset the vertical stab.  Here's my reason.
 
1. Any fixed trim is generally only good for one airspeed and power setting, so unless you never intend or think your gear box, prop or engine is going to change I wouldn't try to compensate with vertical stab.  Once it set, it a lot of work to change.
 
2.  Cockpit   trim is of course the ideal, but then you may have to rig up something to drive the trim tab, worry about what that might do to flutter points, etc. this one takes time, money and effort to get it right.
 
3.  An adjustable trim (such as a rudder trim tab) can be adjusted to take care of such changes as mentioned in 1 above
 
All in all, its hard to beat a trim tab for adjustability, weight, cost, and ease of application and since a vertical stab orientation or a trim tab are both only idea for one airspeed and the tab is much easier to adjust - I would vote for it.
 
Years ago someone told me he was going to design his vert stab like an airfoil. The idea being that as the airspeed varied the "lift" of the vert stab would change.

Finn
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