trim tab profile

The place to raise issues, ask questions, swap ideas and discuss anything related to aircraft engineering, maintenance and building.
NB Any opinions expressed in this forum are not necessarily those of LAA Engineering

Moderators: John Dean, Moderator

Post Reply
rans6andrew
Posts: 63
Joined: Fri Jul 17, 2009 3:39 pm

trim tab profile

Post by rans6andrew »

I have noticed that the in-flight adjustable trim tabs on some aircraft are not "razor sharp" along their trailing edges but have been deliberately made with a lip on both faces. They seem to be made from a double thickness of sheet aluminium and the edges are splayed apart for the final quarter of an inch (6.4mm) at about 90 degrees. Is this done for some aerodynamic reason or is just to stiffen the edge?

Anyone have further to add?

Thanks,

Andrew Cattell
David Hardaker
Posts: 70
Joined: Fri Jan 04, 2008 6:18 pm
Location: Yorkshire

Thick t/e

Post by David Hardaker »

AIUI it's to reduce the "dead" band around neutral...
d
gasax
Posts: 165
Joined: Wed Jan 09, 2008 12:43 pm
Location: Aberdeen

Post by gasax »

It reduces the tendency for flutter to occur by always ensuring that the airflow from the rear of the tab detaches in the same place.

(FWIW the original Sierra had issues in crosswinds for exactly the same reason, the slipstream detached at different points depending what the crosswind was - giving a tendency for it to wriggle. This was 'fixed' by small spoiler on the rear most window surround!)
Pete Morris
013242
Post Reply