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Discussion has been un-focused on the result of taking the flaps "out of
Reflex", etc.

Is there anyone out there that can provide repeatable, verifable data
concerning the relationship between flap position (10, 30 and 45
degrees) and lift versus drag on the Lancair 320 wing?

Why do we use 10 degrees of flap for takeoff (as per  the POH)?

Scott Krueger
N92EX

Note:  The Messenger (Tom Giddings) is not responsible for the queries
proffered  in this missal.

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