Mailing List lml@lancaironline.net Message #51695
From: Frederick Moreno <frederickmoreno@bigpond.com>
Sender: <marv@lancaironline.net>
Subject: FW: [LML] Re: L360 winglets
Date: Mon, 08 Jun 2009 13:00:03 -0400
To: <lml@lancaironline.net>

“There is absolutely no question that winglets work if properly designed and correctly installed.”  

 

It depends on what you mean by “winglets work.”

 

Winglets can reduce induced drag at the expense of an increase in parasitic (friction) drag arising from more surface area exposed to the flow.  The result is a net decrease in drag if you fly with a lift coefficient greater than about 0.5-0.6.  That corresponds to high angles of attack.   In airliners, it means travelling heavily  loaded up high in thin air where the airplane is mushing along.

 

Since we fly our airplanes in regimes where the lift coefficient is more like 0.2-0.3 (in thick air going comparatively fast), the reduction in induced drag is slight while the increase in parasitic drag is more than slight, and consequently the airplane goes slower.

 

If you want to fly your Lancair slowly like a glider near it’s best lift/drag speed (about 135 knots IAS in a Lancair IV), there will be measurable performance benefit with winglets. 

 

As you go faster, the drag reduction benefits of winglets decline and become negative as you approach cruise speeds.

 

As for appearance, ah, that is a subjective, not quantitative, assessment.

 

Wingless Fred

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