This reminds me of a discussion in the early days of altimeter use in in NAR competition, with porly worded rules. I suggested that the altimeter could be ported to a low pressure region of the airframe, producing higher altitude readings than those taken at true apogee. I suggest the altimeter could be ported to the convex corner of a conical transition. To drive home the point, I suggested that altimeter could just be ported to the throat of a venturi. They finally adjusted the rules.
So, my question is, how would you design a venturi into or around a contest rocket to maximize the "altitude" reading of the altimeter?