Originally Posted by
RetiredF4
It is based on my own expierience out of high performance aircraft with a big ugly stabilizer....... which we could stall at less angle than 45° AOA. Fortunately we had a big heavy cannon in the front with lots of weight and favorable cg.
So it would be kind if you could proof it with numbers for the AF 447, otherwise its just an oppinion of yourself.
franzl
Although in an F-4 with its tiny VS and the Anhedral/Dihedral I would assume the main danger was not so much the stall itself but the spin.
With the CG and aerodynamic Design of it I would expect rather swift Nose Drop at the Stall. The thrill being not to spin it (unrecoverable?) and therefore not to drop a wing.
Am I right ?