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The following passage from Flugbericht Fw190 410230 V 34 Nr.1 should be kept in mind when discussing Fw 190 flight test figures from Focke-Wulf Flugzeugbau:
Ergebnis zu 1) Erstmalig ist im Kurvenblatt 1) die über der Meßstrecke ermittelte Staudruck eichung unter Berücksichtigung der Kompressibilität der Luft aufgetragen. In Zukunft werden alle mit den BMW 801 F und Jumo 312 Triebwerken ermittelten Geschwindigkeitsleistungen mit Berücksichtigung der Kompressibilität bekanntgegeben. Bei den Flugzeugen mit 801 D Motoren entfällt diese Umrechnung auch weiterhin, um die Vergleichsmöglichkeiten mit früher ermittelten Werten zu erleichtern.
That said, the comparison discussed in the report on Fw 190 528 is very interesting and worthy of note.
I always wondered what would be the performance of the A4 airframe in combination with the later BMW 801s of the 2100 ps. It would be an excellent vertion for the Eastern front. But the RLM could think of nothing else than more and more guns and more and more armour
Once again, as in the case of the Me 109, RLM was unwilling to insert improvements from fear of losing some production
Producing masses of aircraft was a far easier thing than producing masses of trained pilots.
This is where the big argument for 'quality over quantity' comes into play to. And while it's certainly true that having a well-organized, efficient training program infrastructure would have made a huge difference as well, the issue of putting an emphasis on war machines able to make the best use of existing high quality pilots/crew is significant. That and putting a greater emphasis on operational effectiveness would be more important than initial manufacturing costs. (ability to fulfill their given mission, survivability, handling on the ground and in the air, reliability, and resources required for maintaining continual operations -man hours spent on maintenance, skilled personnel required to maintain the machines, as well as material resources of oil, fuel, spare parts, tool wear, etc)For the Fw 190 (and other A/C) to remain competitive, an improved engine is needed at least every year, ie. from late 1943 the substantially better engine is needed, after the fully rated 801D (late 1942) and the start with 801C (late 1941 in combat). The 190 got it in late 1944 instead, LW lost the air war in the mean time.
Producing masses of aircraft was a far easier thing than producing masses of trained pilots.
When the escorts showed up, the twins were outclassed and could not survive long. I'm not sure the Fw 187 would have been that much different.
Would someone please tell me what happened to the Fw 190 B? Why was it cancelled?
The Daimlerized Fw 187 vs. the Fw 190 - it depends what we want from the aircraft, and what engines are available. If we want the aircraft with 4 cannons (or more?) and plenty of fuel, the Fw 190A becomes a non-performer - the Fw190A-8. The Fw 187 with ~3000 HP (talk DB 605A, late 1943 on) can lug around a heavy battery of cannons and plenty of fuel, and still perform. From mid 1943 on, the Fw 190 needs the engine better than the BMW 801D, lets say the Jumo 213 or DB 603 in order to match it, and here the LW dropped the ball in crucial time of war.
Dietmar Hermann, in his booklet about the high altitude Focke Wulf fighters, says that there are no clearly stated reasons about why the 190B was cancelled. He also writes that Kurt Tank didn't liked very much that the weight of the 190B was increased by 150 kg because the GM-1 system was to be installed. One of the features to be incorporated in the 190B was the bigger wing, 20.3 sq m vs. usual 18.3.
The 190B-1 was stated in RLM production planing, production was to start from June 1942, with 2991 fighter planed to be produced until Dec 1943.
The 190B was turbo-charged. They couldn't afford the metals to build turbochargers in that quantity, so they cancelled it, just like the they didn't build the Jumo 004A or the turbocharged Fw190C.Dietmar Hermann, in his booklet about the high altitude Focke Wulf fighters, says that there are no clearly stated reasons about why the 190B was cancelled. He also writes that Kurt Tank didn't liked very much that the weight of the 190B was increased by 150 kg because the GM-1 system was to be installed. One of the features to be incorporated in the 190B was the bigger wing, 20.3 sq m vs. usual 18.3.
The 190B-1 was stated in RLM production planing, production was to start from June 1942, with 2991 fighter planed to be produced until Dec 1943.
The 190B was turbo-charged. They couldn't afford the metals to build turbochargers in that quantity, so they cancelled it, just like the they didn't build the Jumo 004A or the turbocharged Fw190C.
Going by this thread, the 190B was not turbo charged: link.
The Jumo 388 used turboed engines, the hollow blades were a way to circumvent the requirements for the rare metals.
The reason why the turboed DB 603 was cancelled for the Fw 190 was the installations' huge drag - the Fw 190 with DB 603A was 30-50 km/h faster from SL up to 9 km, the turboed 190 taking over above 10 km. The Fw 190 with DB 603A that featured the experimental 'G' (scroll type) supercharger was faster up to 10 km, and above was equally fast.
Going by this thread, the 190B was not turbo charged: link.
The Jumo 388 used turboed engines, the hollow blades were a way to circumvent the requirements for the rare metals.
The reason why the turboed DB 603 was cancelled for the Fw 190 was the installations' huge drag - the Fw 190 with DB 603A was 30-50 km/h faster from SL up to 9 km, the turboed 190 taking over above 10 km. The Fw 190 with DB 603A that featured the experimental 'G' (scroll type) supercharger was faster up to 10 km, and above was equally fast.
Für die B-Baureihe der Fw 190 war ursprünglich der BMW 801 J als Antrieb geplant (der später in wenigen Exemplaren auch in der Fw 190 A-9 verbaut wurde).
Da der BMW 801 Motor ursprünglich nicht für den Einsatz in einem Jagdflugzeug entwickelt worden war, verfügte er auch nicht über einen Lader, dessen Leistungsfähigkeit in größeren Höhen mit jenem z.B. des DB 605 V-Motor [1] vergleichbar war, der der Messerschmitt Bf 109 gegenüber der Fw 190 A eine deutlich bessere Höhenleistung verlieh.
I'm not referring to the turboed 190C - there was no such thing? The 'turboed' Fw 190 was the V18/U1 (Wk.Nr.0040), and it was one draggy aircraft. Same the for similar machines - from V29 to V32.
The V13, V15 and V16 (DB 603A, but no turbo) were far more streamlined practical aircraft, without the inter-cooler's radiator and turbine sticking in the slipstream in 1920s/30s fashion. V15 was later used as trial machine for the installation of turbo-associated plumbing.
The more streamlined turbo installations, that required cutting a bit of the fuselage fuel tankage so the turbo and inter-cooler can be buried in the fuselage, never left the paper stage.
Was the turbo worth the drag?
Could it have been made more aerodynamic?
How much speed did it sacrifice?
As flown - a clear 'no, it was not'. It could, at least if we look at the drawings of proposed semi-buried installations, that never past the 'paper stage'. Inter-cooler, turbo and tubing cost 30-50 km/h from SL to 8 km, less between 8 and 9 km of altitude where the turboed DB 603 have had a hefty power surplus vs. the 'normal' DB 603 to overcome the drag.