Hi all, Just a generalised question about rolling moments generated by an aircraft with a dihedral wing during sideslip. Are there any equations which relate (generalised) the sideslip angle of an aircraft with a dihedral wing and its rolling moment? I would like to be able to calculate the amount of roll generated as a result of some degree of sideslip induced by rudder action alone. I would, inevitably, want to use this roll angle to calculate the turning angle and rate of an aircraft. But prior to that, I want to be able to calculate the amount of rudder (and induced sideslip) which will result in a specific bank angle. Ideas? Inspiration? Any recommendations for books for beginners in this field? Thanks!