Sorry, no numbers, but I can say that it gets very complicated on something like the shuttle carrier (there's gotta be a good nickname for that thing) or an E-3. The strapped on bits for those aircraft are mounted at an AOA designed to give neutral lift (i.e. lift equal to their own weight) at cruise. CG doesn't change, obviously, but I wouldn't even know where to begin with the stability side of things.
Edit: Sorry, I just thought about that for a minute. I know the neutral lift statement is correct for the E-3, but obviously, for the shuttle to be hauling it's own weight at whatever the cruise for the carrier turns out to be, it's AOA would have to be in the 10s of degrees. See, I don't even know where to begin thinking about where to begin.