If our engine is the Jumo 213A, the annular radiator is for the engine coolant. Only a single coolant port at the top and two at the bottom. The coolant and oil was kept at high pressure like in the DB60X engines so their boiling point would be kept high as altitudes increased. If not pressurized, liquids boil at a lower temp as alt increases.
With a 1 : 2 radiator port arrangement to service two banks of cylinders under pressure. Damaging either side is moot. Your pressure will drop and your feed will eventually run out the hole. If you look at the engine's cutaways and cross sections. It's a high pressure oil leak waiting for the first API, 20mm, or 30mm round to breach the block\cylinder heads or to crack it. If you put enough armor plate around the whole engine to make it API\cannon proof, look at maybe the SL WEP speed as your overall alt top speed. The armor in the annular ring is betting on the bullet path to strike at an angle compounding the relative thickness of the plate.
It's a big toe waiting to get stubbed on a rock except where the engine mount arms are. Everything else will get broken or chewed up. Lots of high pressure tubing and feed lines to shred.
If it's the DB603 it's got the oil cooler sitting on top of the reduction housing as a small oil cooler box and the coolant radiator laying in the lower part of the annular housing ring. Another big toe waiting to be stubbed along with the engine block.
Back to my questions.
1.- Is this an area effect calculation needing the forward region pulled back to the annular ring?
2.- Is this a bug?
3.- Is this a test of your reactions to the reality of how vulnerable inline engines were in WW2 for future considerations to realism?
So are all of our inline engines equally vulnerable except with the IL2?
Link to one of the JUMO 213A D9 manuals:
http://www.scribd.com/doc/122004586/focke-wulf-fw-190-d-ersatzteil-liste-konstruktionsgruppe-6-triebwerk-oktober-1944