Hi,
I would like to address the points made by F4UDOA.
Originally posted by F4UDOA:
Andy,
It is an excellent piece of work. Based on this the Max sustained turn is at a much higher speed than your friends graph. I believe that it is too low because even though your friend is close on the 1g stall of a P-51 in the clean condition he is off on the 3G turn being at less than 150MPH. The Mustangs 3G stall based on the 1g stall is 181.86MPH or 105MPH*1.73(The square of the G factor). The 105MPH stall is from the P-51 Flight manual. In any case the graph is beautiful. I will get my Physics tutor to check the thread and give his two cents.
F4UDOA
The diagram posted was for the P-51D as modelled in Air Warrior. What it shows, is exactly what happens in that simulation, as such it is valuable to the good folk who fly that sim'. However, while it is a 100% faithful indication of what happens in that simulation, in that configuration, the information is non-transferable. It can't be used for other simulations, or for the real world aircraft, although it could be with some adjustments. So, the lift curve used to generate that diagram doesn't reflect the lift curve of the real P-51D it matches the curve used to model the P-51D in Air Warrior. Also, the prop efficiency curves don't match those of the real P-51, and the engine power curves don't match either. For example, the value of Clmax reflected in the Air Warrior simulation (that is the highest point on their lift curve) is 1.56, the value for the real P-51D is 1.89. I believe the difference is due to the fact that the guys at Kesmai probably used airfoil data, which is almost always somewhat less than the values realised by the complete aircraft in flight.
Regarding stall speeds, much care is needed when quoting specific values. For example, the weight of the P-51D could vary from a maximum take off weight close to 12,000lbs to as little as 7,300lbs when landing on fumes with no fuel and a hungry pilot. That results in a stall speed at sea level and standard atmospheric conditions ranging between 70kts (81mph) and 90kts (105mph) which probably explains why the P-51 flight manual quotes the high end value. Following that reasoning through yields 3g stall speeds ranging from 121kts (140mph) to 156kts (182mph)… The point is that the diagram posted is correct for the configuration it represents, just as your figures are also correct.
Hope that helps?
Badboy