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Thanks for the info
My google-fu has yielded some results, the AM-37 seem like a winner ( but, according to Russian Wiki, it was prone to overheating). Sorry for the low-res graphs; the AM-39 and later are not for this thread really:
In what altitude the AM-38 achieved that power? IIRC it was a low-alt development of the AM-35. Maybe it was unfortunate for Soviets that a 'mid-alt' version of either the -35 or -38 was not produced; the AM-37, an alternative, being prone to overheating.
At SL boosted for T.O.
Nice job.
The book on Russian engines says that they could not get to the "required level of reliability" which, considering the life of the AM-35, is saying something. It also says the aircraft designers could not cope with the cooling problems but does not go into details. I may be guessing to much but if it is the aircraft designers and not the engine designers then it sounds like the radiator and inter-cooler installations were giving trouble. Intercooler was an air to liquid intercooler like on the Merlin. Too much drag?
I suspect that's why the Soviets were happy to acquire P-39s and P-40s during 1942. Better then anything they could build while Soviet industry was in turmoil.too much to ask from Soviet engineers to solve the issue, because of German onslaught, factories labs relocation etc.
T-34 production quality was horrible during 1941 and 1942. Give me a reliable Lend-Lease Sherman any day of the week.