Flap Type and Efficiency

[hitech]

Hitech
I posted in haste I should have rephrased my question. I thought I was asking if you modeled the tail plane forces without the effect of the down wash from the main wing.

Edit: Slightly off topic. I believe you model spiral slipstream on the tail, is it possible when slow at a high AOA to drop the tail out of the slipstream?

We do model wing blanking FLS.

HiTech

[Stoney]

We do model wing blanking FLS.

HiTech

That's cool to know...another feather, so to speak...

[thorsim]

pretty sure WB pitches down ...

[Ex-jazz]

<snip>"effect of the down wash from the main wing."<snip>

How the wing down wash is effecting to the tail (elevator) during the turning?

The tail AoA is increasing/decreasing?  

[hitech]

That's cool to know...another feather, so to speak...

We also model the change in The LCO do to the speed of an AOA change. I.E. basically increasing camber do to a changing AOA.

HiTEch

[Soulyss]

Whenever I try to read these threads about flight modeling and principles of aerodynamics, especially when terms like CL and CM curves, AoA, LCO, and Camber start getting tossed around I'm reminded of the following bit, it's right around the 1:15 minute mark.

http://www.youtube.com/watch?v=3mJoHqmtFcQ&feature=related