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I see that in my reference above, it is said to have been completed with the DB601s but there are no performance numbers. According to another source, it achieved some 391 mph but, in service, the use of conventional radiators would have slowed it to 348 mph, so it was discarded. Another reference, German Aircraft of the Second World War by Kay Smith says it had DB 600 engines, not DB 601s, and that it was deemed "unsuitable."
So ... I overlooked the V5 in my first post and cannot find any two references that agree on either performance or engines installed ... other than the dates when it was accepted, Aug 1940, and the when taken out of service, July 1941, and parked.
I have no record of flights completed in any of the references.
It certainly LOOKS like a potential winner, but so did a lot of other potential service aircraft that were not eventually accepted into service ... on both sides. Maybe the radical cooling system was its downfall because it showed very promising performance until conventional radiators were needed. Then it's predicted performance became rather ordinary, speed-wise.
Maybe they didn't look much at handling when the projected top speed didn't represent a jump in performance in that category.
The reason Kurt Tank wanted to use DB600/601 was that they had pressurized cooling circuits which made them suitable for evaporative skin cooling which was all the rage for a while, Mitchell even tried it on the progenitor for the Spitfire. Neither the Jumo 210 or early Jumo 211 had a pressurized cooling circuit. Nevertheless the small Jumo 210 (21 Litres) using only radiators was still 100kmh faster than the Bf 109D which used the same engine.
The idea with a evaporative skin cooling is to take the pressurized hot water from the engine, allow it to flash into steam, then use a centrifuge to separate out any water, then to condense the steam to a liquid in the skin of the aircraft eg the leading edges. Scavenge pumps than collect the water.
Fw187 CI+NY (WkNmr 1976) was fitted with DB engines and flown late 1939 onward. While it proved to be fast, it was prone to skin buckling and cooling problems. Last mention of it was 1942.
I see two supercharger drive ratios for the -22W and -34W, but am not immediately aware just now if those are 2-stage or 2-speed. I very rarely memorize engine variants. Too easy to get it wrong in your mind.
I can certainly look it up, but wasn't in the mood to dig this evening.
Being a Navy plane, it makes sense to have a single-stage, 2-speed engine, but things don't always follow the sensible route ...
If I get a chance to work on a Bearcat or Tigercat, it would most likely not be an engine anyway. It would be sheet metal, systems or landing gear. I could do more, but Tigercats are privately owned these days and the owners are picky about who does what.
If I had one, I would be, too!
The USN was on forefront of 2-stage engines' development, two P&W engines were used on a wide sclale through ww2, while one Wright R-2600 with 2-stage S/C powered the 1st Hellcat's prototype. USN was never in the turbo business, they believed more in the engine-driven 2-stage systems.
Note the author offers no evidence of having DB 601 engines actually installed, he just asserts that it was designed for them. There are numerous instances of aircraft being designed for an engine only to be fitted with something else. The Bf 109 prototype was fitted with a Rolls-Royce engine when the intended engine was not available. After reading this carefully, I now discount his assertion that the V-5 was equipped with DB 601 engines because not one shred of evidence is provided except his assertion that it was designed for DB 601s. That isn't evidence that it ever happened.
You say the author states that speed was at sea level; that is incorrect. He states it was achieved "at low level" on page 78. He makes no mention of the flight being at sea level at all. He DOES say the DB 601s could produce 1,350 HP for one minute at ground level, but that in no way implies the flight was made at sea level, it only tells us the power that the engine could produce at "ground level" which, in Bremen, is quite low but is not at mean sea level.
Your "SENTENCE" above does not appear in my English language book. Yes, he states what engines he believes were installed, but there is not one shred of evidence it was ever done or ever flew. They actually installed the DBs in the V6 and there is a pic of it, but they were removed later, when 80% complete, and when it flew, it flew on Jumos.
Please keep discussion civil.
Please keep in mind that some detail information may be lost in translation if it wasn't done 100% correct.
Th To me GregP has a clear agenda and implies that Mr. Herrmann provides opinions and lies instead of proves.
Good post Denniss.
I just saw Joe's post above, so my response is not needed to further this discussion.
If anyone has other references for the Fw 187, maybe share them? This is a fascinating plane that probably should have been acquired by the Luftwaffe early in the war but, for some reason or another, wasn't. It might well have been the "Destroyer" they were searching for all along, had it been placed into service.
Sorry DonL,
The "V6" above is a typo and should have been "V7" on page 81. My fault there. I DO make the occasional, or not so occasional, typo. Generally, great pics in this book. I particularly like the one on page 45 showing the Fw 187 in the inverted position. I'd like to find that one in high-resolution format, but it is unlikely.
Actually, only one typo for me is pretty good!