Jeff,
It is great to see members of our community pushing the envelope and continuing to experiment in an effort to improve CFS 3 for all of us.
I will share some thoughts with you that may help you with your work. I have logged close to 5,000 hrs mostly SEL with some turbocharged engines.
1. Airspeeds IAS(Indicated Air Speed) vs TAS(True Air Speed) - Most published airspeeds in aircraft performance are listed as TAS at altitude while IAS is used for manuvering, stall, gear and flaps. The cockpit ASI should always read IAS.
2. Indicated airspeed drops off steadily as altitude is increased due to air density. It is noticeable even at crusing altitudes under 10,000 ft in light aircraft. For example a TAS of 400 mph may only generate a IAS of 325 mph at 30,000 ft.
3. Turbo chargers and Superchargers will only maintain a certain pressure altitude and cannot generate sea level pressure at high altitudes. Therefore I would refer to the published data for the aircraft in question to match the cockpit MP with the accurate data at a given power setting and altitude. I know that my Cessna 180 at 7,500 ft would only generate 23 inches of MP at full throttle. It would cruise at 155 MPH TAS with a IAS of about 140 mph.
4. The reason that aircraft fly faster at high altitude is less lift/drag, as the air becomes thinner there is a formula for calculating the changes in the lift/drag ratio for a given aircraft at various altitudes.
5. Propellers loose a lot of performance at altitude and there are also formulas that model this as well.
6. Finally weight affects the flight performance of an aircraft as well as external pylons and weapons. The O-1 was severely affected when loaded with 2.75" rocket launchers.
I hope all of this helps as Gregory and I had a lot of discusions in the past on these issues as he built his 1% models.
Keep experimenting and working away, just remember that FMs are the most complicated thing you could have chosen.
Best Regards
Steve