Jon S Berndt wrote:
On Thu, 13 Mar 2003 22:26:31 +0100
 Erik Hofman <[EMAIL PROTECTED]> wrote:

They encountered a problem where the aircraft could fly past 2 degr. aoa. It took them quite long to learn that the wing root of the F-16 (the part of the fuselage that extends to underneath the canopy and where the wings are attached to, but not from the wings itself) was actually an airfoil contributing highly to the lift!


The "strake"?

That one.


Erik


_______________________________________________ Flightgear-devel mailing list [EMAIL PROTECTED] http://mail.flightgear.org/mailman/listinfo/flightgear-devel

Reply via email to