Huh?
One of the secrets of the Me109 is its wing. A unique design like no other.
"I was particularly interested in the operation of the slats. the action of which gave rise to aileron snatching in any high-g manoeuvres, such as loops or tight turns."
"A number of dummy attacks on a co-operative Lancaster and a friendly skirmish with a Mustang flown by one of the RAE pilots revealed the fact that the slipstream of these aircraft caused the intermittent operation of the Bf 109G's slats so that accurate sighting became an impossibility."
"At its rather disappointing low level cruise speed of 240 mph (386 km/h) the Gustav was certainly delightful to fly, but this situation changed as speed increased; in a dive at 400 mph (644 km/h) the controls felt as though they had seized!"
With the same power in the Me109 and an empty weight of 1,700 lbs. less, the climb rate of the Me109 was substantially higher than that of the P-51. Because of the fantastic handling characteristics of the Me109, the P-51 was not match for the Me109.
"The Mustang III possessed a clear speed advantage at all altitudes, this ranging from around 30 mph (48 km/h) at the Bf 109G-6's rated altitude to some 50 mph (80 km/h) at 30,000 ft (9 144 m). The Gustav offered marginally better climb rate up to 20,000 ft (6 096 m) but between this altitude and 25,000 ft (7 620 m) the Mustang had a very slight advantage. When dived and then pulled up into a climb there was little to choose between the US and the German fighter, but the Mustang could steadily out dive the Bf 109G-6 and had no difficulty in out turning the Messerschmitt."
The performance of the Me109 and the Spitfire is almost the same. However, the Spitfire had an average 25%C plain aileron which, despite differential control, gave it a very heavy stick force in roll compared to the light stick force of the Me109.
"The Air Fighter Development Squadron flew the Bf 109G-6 for tactical trials with a Spitfire LF IX, a Spitfire XIV and a Mustang III (P-51C) and found thast the first mentioned type had a slight speed advantage up to 16,000 ft (4 877 m) when using 18 lb (8.16 kg) boost, but the situation being reversed between this altitude and 20,000 ft (6 096 m) at which the Spitfre LF IX regained the speed advantage to the extent of some 7 mph (11 km/h). Using 25 lb (11.3 kg) of boost the Spitfire proved to be about 25 mph (40 km/h) faster below 15,000 ft (4,570 m) and around 7 mph (11 km/h) faster above this altitude, which climb was superior to that of the Gustav at all altitudes and particularly below 13,000 ft (3 960 m). The Bf 109G could leave the Spitfire LF IX behind in a dive without any difficulty, but when both aircraft were pulled up into a climb from a dive their performance was almost identical, the Spitfire slowly pulling away as soon as climbing speed was attained."
With a 50% span and narrow chord, Frise, aileron, the Me109 stick forces were very low in roll and it could roll quicker and was more evasive than the Spitfire which was slow in roll.
"The rolll rate and turning circle of the British fighter was very much superior at all speeds."
The control harmony of the Me109 could not be matched by any Allied aircraft in WWII.
"Control harmony was poor for a fighter, the rudder being light, the ailerons moderately light and the elevators extremely heavy."
Information courtesy of Eric Brown from Wings of the Luftwaffe.