I remember an episode on the History Channel or similar. A WWII pilot mentioned a suprising possible fact about the 51 (may apply to other planes as well). He said if the 51 took a radiator hit. The 51 would only fly for about 45 min and then the engine would freeze. No doubt he could be very much off and may have never experienced 1st hand a radiator coolent hit. His memory from 50+ years ago could be affected as well.
I also remember watching accounts on the 51 having multiple radiator shutoff valves. One of the designers spoke of his experience when designing the 51 radiator with auto-shutoff valves. These valves (didn't say how many) would close if loss of pressure/coolent in a section of the radiator. The idea was in case a projectile (small stone, bullet, etc...) punctured a section of the radiator the plane would still be flyable.
Another thing to keep in mind for overheated engine lockup. My thought is an engine will lock up only after oil loses its viscosity. At various temperatures oil will break down over a given amount of time. The hotter the oil the faster it breaks down. So for example, the current AH2 engine rise model may be accurate to some extent. Meaning, after the engine temp goes into the red zone. The oil is shot and results in extreme friction and heat gain. Another factor in determining engine heat/loss effect is the oil cooler radiator. The oil cooler would aid in cooling an engine as well, but with limited results.
I would like to suggest the following if coolent loss time/engine overheat lock-up is re-modeled:
1. The engine temp. gauge seems to rise the same no matter what the engine throttle is set to. I believe engine temp. rise should be based more on throttle position and maybe even RPM’s.
2. The engine temp. gauge seems to follow a linear heat rise instead of exponential. As an engine gets hotter, heat would radiate off the engine at a higher rate than at lower temp's., thereby, slowing the temp. gauge rise as the engine temp. nears the red zone. This is basic 101 thermodynamics which state heat transfers at a linear rate with regards to delta T (delta T = the difference in temperature between two objects or mass, the higher the temperature difference = higher heat transfer rates).
I suggest the following (for a rough example only) that engine temp. gauge should do the following with the loss of liquid coolant. Note: this is just a guestamate.
Proposed engine temp gauge rise rate with no liquid coolant and at full throttle (degrees C):
From 90 to 100 = 0.5 minutes
From 100 to 110 = 1.25 minutes
From 110 to 120 = 2.5 minutes
From 120 to 130 = 4.0 minutes
Proposed engine temp gauge rise rate with no liquid coolant and engine off (degrees C):
From 130 to 120 = 1 minutes
From 120 to 110 = 3 minutes
From 110 to 100 = 5 minutes
From 100 to 90 = 8 minutes
Please don't take my word for the above suggestions. These are things I would be interested to learn in more detail. My above suggestions may 100% wrong do to oil viscosity breakdown effects. Who knows, the current AH2 coolent loss modeling may be accurate as-is?