Hi Claidemore,
>Note that the P40 could pull 5 g at 180mph
Hm, at which weight? The G rate appears to be a bit on the high side - I have the P-40 maximum coefficient of lift as 1.45 (from Peril's data), and that would require a weight of no more than 3180 kg at 200 mph (the upper limit of the range given in your quote).
>while the 109 E was stalling at 3 g at that speed, according to RAE tests.
Hm, if you you refer to the Spitfire-vs.-Me 109 turning diagram dated 19-11-1940, it shows about 3 G at 200 mph TAS, but I believe it would actually have be read at the 200 mph IAS reading for a comparison, and there it gives about 4.5 G for the Emil. The latter figure is also in fairly good agreement with my calculations.
Regards,
Henning (HoHun)
>Note that the P40 could pull 5 g at 180mph
Hm, at which weight? The G rate appears to be a bit on the high side - I have the P-40 maximum coefficient of lift as 1.45 (from Peril's data), and that would require a weight of no more than 3180 kg at 200 mph (the upper limit of the range given in your quote).
>while the 109 E was stalling at 3 g at that speed, according to RAE tests.
Hm, if you you refer to the Spitfire-vs.-Me 109 turning diagram dated 19-11-1940, it shows about 3 G at 200 mph TAS, but I believe it would actually have be read at the 200 mph IAS reading for a comparison, and there it gives about 4.5 G for the Emil. The latter figure is also in fairly good agreement with my calculations.
Regards,
Henning (HoHun)