I am curious about the engines that each kind of aircraft carried in AH. For example, the Spitfire MkIX had 4 different engines. I'm sure that other aircraft follow the same pattern.
What I'd like is for those who know about these things, for any aircraft, and who know the engine modeled for the AH version of the aircraft to post the pros and cons of each engine for that aircraft. If possible indicate how many aircraft of the types used each engine.
I'll start with a few British aircraft.
Mosquito Mk VI
The Mosquito FB.Mk VI used three different engines, the Merlin 21, Merlin 23 and Merlin 25. I am unsure on the differences between the Merlin 21 and 23 as I have always seen them listed as producing the same power, there may be altitude performance differences. The Merlin 21 and 23 produced 1,230hp. The Merlin 25 produced 1,635hp. The advantages of the Merlin 25 are obvious.
The majority, my a good margin, of Mosquito VIs were equipped with the Merlin 25. I have never been able to find actual numbers, but the impression I get is that only those Mosquito FB.VIs originally ordered and Mosquito B.IVs were equipped with Merlin 21s or 23s.
The Mosquito Mk VI in AH is equipped with the Merlin 25, the best available engine and the most representative.
Spitfire Mk IX
There were four different engines used in the Spitfire Mk IX series, the Merlin 61, Merlin 63, Merlin 66 and Merlin 70. The Merlin 61 was the first 2 stage Merlin engine and produced the least power of the various Mk IX engines. The Merlin 61 is tuned for high altitude performance, only obtaining 321mph at sea level but managing a respectable 408mph at 25,000ft. I know little about the Merlin 63, and it doesn't appear to have been used on many Spitfire IXs. The Merlin 66 was a two stage Merlin tuned for lower altitude performance and producing more power, reaching ~335mph at sea level and 404mph at 19,500ft and a very good 372mph at 8,200ft. The Merlin 66 also increased the climb rate significantly. The Merlin 70 was the high altitude tuned counterpart to the Merlin 66.
The first 300-400 Spitfire IXs were equipped with the Merlin 61. Approximately 70% of the 5,665 Spitfire Mk IXs produced were powered by the Merlin 66, in addition all Spitfire Mk XVIs (basically a Spitfire Mk IX powered by an American built Merlin engine) were powered by Packard Merlin 266s, the American version of the Merlin 66. Most of the remaining quantity of Spitfire IXs were powered by the Merlin 70.
The Spitfire Mk IX in AH is equipped with a Merlin 61, the worst available engine, save that the AH Merlin 61 does not have a float carburator.
Seafire Mk IIc
The Seafire Mk IIc was powered by two different engines, the Merlin 45 and Merlin 32. Early Seafire IIs were powered by the Merlin 45, which was tuned for optimum performance at 13,000ft and produced ~1,440hp. The Merlin 32 was a low altitude tuned Merlin producing 1,645hp. Merlin 32 equipped Seafire IIs mounted a 4 blade rotol propeller, were significantly faster and had a greater rate of climb.
The majority of the 372 Seafire Mk IIs were powered by the Merlin 32.
The Seafire MkIIc in AH is powered by the Merlin 45, the less effective of the two.
I have heard that the Typhoon in AH has a more powerful engine that earlier Typhoons, but all my references only mention the Napier Sabre II at 2,180hp, the same engine as on the Tempest. They do mention chages in the propeller and conckpit, but no engine differences are discussed. Somebody with more knowlege about Tiffies will have to clarify that.
So, lets have the data for some other aircraft.