posted on Oct, 22 2019 @ 01:24 PM
originally posted by: anzha
a reply to: Zaphod58
There might be a necessary reassessment of the maneuverability of the J-20.
I don't think so, unless you had a very poor opinion of the maneuverability in the first. It also reflects the emphasis on supersonic performance and
RCS-reduction.
If you look at the apparent center of mass/lift, the moment arm for the tail is not very long. That's why deltas frequently sport (seemingly)
oversized vertical stabilizers and rudders. The choice of an all-moving rudder is in part due to that. An all moving rudder generates more force than
a small rudder on the stabilizer, which allows them to get the stabilizer surface(s) smaller than otherwise.
That also means it can make smaller deflections to further minimize changes to RCS in cruise. It also doesn't have gaps for the hinges on a
conventional rudder which would raise RCS in certain bands (see all-moving ruddervator for the YF-23 design, Tacit Blue, all-moving ruder for F-117,
Su-57, etc). You also get lower waveform drag at supersonic speed from a single flat surface than a tail with a hinged control surface (see the
Blackbird/Archangel family, Vigggies, YF-23, Su-57).