PPRuNe Forums - View Single Post - Static longitudinal stability - converting airspeed to lift coefficient
Old 13th July 2018 | 15:09
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Downwind Lander
 
Joined: Apr 2014
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From: London
Originally Posted by Genghis the Engineer
That's a very odd interpretation. Most of us class lift as the total net lift from wings, surfaces and airframe - not just the wing.

G
I wonder if Dook means that the elevator produces downforce (or upforce) whereas the tailplane produces lift (which is what you are saying, G, in slightly different words).
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