Hello,
Reading a bit about the Bf 109F, it seems that the 109F-4 introduced, after a small number were delivered, the air intake duct of increased size/area. The new duct provided better use of ram effect vs. the old, more restrictive one found in earlier 109Fs. The aircraft top speed was at altitude that was 1100 m greater than engine's rated altitude, on Kampfleistung (1400 m for Notleistung).For the 109F-1/F-2, the difference seem to be at ~700m (Notleistung; 2600 rpm 1,42 ata)? End result was the Bf-109F-4 having the max speed of 635 km/h at 6 with 1185 PS used (= Kampfleistung) vs. the Bf-109F-1/F-2 with 615 km/h at 5,2 km/h with 1200-1250 PS.
(both aircraft have had also greater power settings, though)
Questions: is there any information of just how big were the air inlets - what size is the throat area of the air inlets?
What about other, comparable aircraft of ww2?
Reading a bit about the Bf 109F, it seems that the 109F-4 introduced, after a small number were delivered, the air intake duct of increased size/area. The new duct provided better use of ram effect vs. the old, more restrictive one found in earlier 109Fs. The aircraft top speed was at altitude that was 1100 m greater than engine's rated altitude, on Kampfleistung (1400 m for Notleistung).For the 109F-1/F-2, the difference seem to be at ~700m (Notleistung; 2600 rpm 1,42 ata)? End result was the Bf-109F-4 having the max speed of 635 km/h at 6 with 1185 PS used (= Kampfleistung) vs. the Bf-109F-1/F-2 with 615 km/h at 5,2 km/h with 1200-1250 PS.
(both aircraft have had also greater power settings, though)
Questions: is there any information of just how big were the air inlets - what size is the throat area of the air inlets?
What about other, comparable aircraft of ww2?