Hi jb,
about 7 years ago I was having a chat with with a young second officer on a SYD-JNB 747 flight. He talked about ground effect of the wing and tail plane and also of the effect on pitch that the increase in power has due to the power plants being so far below the centre line. He mentioned take off and landing as the most notable times for this. I would be most appreciative if you could share your knowledge on this. As always thanks for the time that you spend both answering our questions and for the wonderful videos you post. As an "aviation enthusiast" I really appreciate it.
Ground effect (aircraft) - Wikipedia, the free encyclopedia
That's a good explanation of ground effect.
In the 747 it was very noticeable, and generally countered with a very slight reduction in pitch and power (half degree, 1%) as you approached the flare. As most approaches are never totally steady state anyway, it just tends to be absorbed into all of the changes that are happening. Do nothing, and the aim point will move further down the runway.
The 380 is even more inclined towards it, but the effect is masked by the flight controls. Generally though, you'll need to lower the nose very slightly from about 250' to hold a fixed aim point.
Ground effect probably saved the Singair 747 that had the massive tail scrape out of Auckland a few years ago.
Pitch couples come into play because the thrust is below the drag line, thus creating a pitching moment. So, increase power and it pitches up, decrease and it pitches down. This is totally masked by the Airbus FBW system...which is great until you have to fly in a degraded mode where it doesn't work. In the 767, the combination of the engines being quite forward slung on the pylons, plus being well below the drag line gives rise to extremely strong coupling.
It is really much the same thing as the yaw coupling that happens on any engine out flying...but in that case the moment arm is across the aircraft. The various moments mean that single engine flying in a 767 was very interesting, with any thrust change causing the aircraft to pitch and to yaw appreciably.