Ok there is a lot of table of speed vs weight vs flaps position everywhere.
I want to compute them and not use any table. And it obvious that tables are the result of some computation.

Do you think I can use something like that ?

Vr = sqr( W / (0.5 * rho(0) * CL0 * S) )
CL0 is CL-0, rho is at airways level.
I think I should add "Delta_Lift_due_to_flaps" to CL0, is this correct ?
If any guru can help me ;)

Something else. I have well advanced with the fmc, you can see a few screenshots here : http://www.chez.com/tipunch/flightgear/index.html

Regards,

Harald.

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