You can't really do 3 bodytubes in OR, but the best compromise is a single bodytube and 2 inner tubes on the outside of the main bodytube. It won't do anything calculation-wise for the aerodynamics, but it will do the engines, mass, and flight calculations. Take the flight calculations with a grain of salt tho', since OR will consider inner tubes as zero drag (since they most likely will be inside the bodytube on most rockets). Anticipate a lower apogee than simulated. The stability factors should be fairly close to reality.