Originally Posted by
markkal
If the ball is kept in the middle, loads will be symmetrical both the wings and fuselage will feel the same acceleration levels.
This is the first time I’ve come across this.
Are you suggesting in the example of a 10 degree nose pitch down upset with significant bank on, that if I roll at the same as pulling up to wings level and an attitude of (around) 0 degrees, and as long as this is in balanced flight, that the G loading on both wings is symmetrical?
Because my understanding is that it is not - and if the upset happened to be a 45 degree bank to the right with significant nose pitch down, that rolling and pulling at the same time towards wings level would result in the right hand wing experiencing a far greater load factor than that of the left hand wing. Hence the need to roll to approximately wings level prior to applying any substantial G loading in the subsequent recovery.
Happy to be corrected though if I have any of that wrong!