I'm thinking the potential for overspeed does exist.
Thanks PJ but I meant it was interesting that the weight loss and CG change weren't modeled in AH. I was asking if, in the case of a wingtip loss, only the drag and lift difference was modeled.
In real life I've never had a prop gain RPM. When hauling jumpers we used a low RPM setting with high airspeed (well, high for a Cessna -- 170 +/-) and didn't notice any RPM change.
Okay. I wasn't sure of your basis. There seems to be a wide range of technical knowledge in this place. Of course, I know you're training staff so I figured you're technically clued in anyway but might like to see those EoMs.
My Grumman had a climb prop and a 160HP conversion on it, and I would have to pull throttle during decents to keep the RPM under redline. Not quite a dive, but once I was showing 150-160 mph IAS, the prop was wanting to turn around 2900 rpm. That being said, I really don't know the overspeed potential of the Jug, just seems like a prop optimized for 300-350 mph wouldn't tolerate that kind of speed. I could be totally wrong though. Bodhi works on them--perhaps he could tell us...
Since you said "climb prop" I'm betting you had a fixed pitch prop in which case RPM will increase with an increase in airspeed.