You'll find this in Timoshenko: Torsion on Thin Walled open Sections
however, does the plane go right through the tube, ie produces two parts of 'C' Section, or only passes through one side of the tube and produce a single 'C' Section. In both cases the maximum shear stress is equal to
Txtmax/J
where J is an integral of (t^3)/3 using polar coordinates and is summed for the arc transcribed.
where T is the maximum torque.
where t is the thickness of the tube.
as the same torque is applied to each part.
If it is one piece the formula is similar, but the integral is summed about the split circle, which means the stresses are generally lower.
When you say, then you stress it, do you mean in bending, because then combined stresses come in to effect where the bending stresses need to be calculate dependant on the postion of the split, only when you have calculated these by general bending theory, can they be combined, generally by St Venants theory to determine the critical stress which can then be compared to the maximum stresses applicable to your particular shaft.
If you could help further by being a bit more specific in terms of dimensions, loads etc, and answer the above queries I could probably be a bit more helpful.
Chris