Originally posted by Karnak:
The N1K2 doesn't have that proble. It is a 5800lb aircraft with a 1900hp engine, it is going to do some incredible manuevers.
Um, other then some microfilm library index card teasers, WHAT data has been checked on the N1K2-J? I do not recall this, other then basic power to weight, wing loading, etc. calculations.
I'd love to see something on it's airfoil preformence, clean and CF's deployed. Brute force doesn't always justify a bad airfoil.

<anal mode>
Its at high speeds were the powered ailerons, overcame high
stick forces, that gave the L model a superior roll rate.
YOKE. YOKE. YOKE.

</anal>
The ultimate reason behind boosted ailerons in the later P-38's was not sole force that had to be excerted to turn the yoke, but the combination of force needed to turn the yoke AND pull it back. In other words, the harder you tried to turn it, the less force you could excerte backwards, due to the nature of the yoke.
Coordination and all that. Bomber pilots had this the worst. Yokes do offer better leverage then sticks as far as roll axis is concerned, but it is VERY difficult to coordinate both control axis' at high speed/forces.

Added smilies. It did look rather anal without them.
[This message has been edited by Jigster (edited 05-30-2001).]