Originally posted by Benny Moore
They're called Fowler flaps, and why would anyone not want to use them? Even the Pilots Manual for the Lockheed P-38 Lightning recommended using the Fowler flaps for turning. A fighter that heavy needs them to be competitive with lighter kites.
I know fowlerflaps, but i never saw fowler flaps that double the liftfactor of a wing without to increase the drag dramatically, but thats what many flaps in AH do and thats why i call them "magic flaps".
Although the fowler flaps was more effective than most other systems, they dont made the P38 to a good sustained turning plane, like it is in AH!!
The P38 was know as a very good B&Z plane and the pilots wrote, "with help of the combat flaps, we could turn inside the smaler planes", to turn inside a plane dont mean to turn with it!!
Imho the AH P38 have a to high E-bleed without using the flaps, what make this "magical flaps" needed to provide a somewhat credible result, while the way to get this result isnt credible.
Same count for the magical F4U flaps, while the F4U without the flaps already show the great realistic advantages of this plane(high speed, good upzoom, good roll), this "magical flaps" in combination with its realistic advantages make the F4U (specialy the -4) to the monster dweeb plane in AH.
btw, this have nothing to do with Luftwhining, the 109F also behave to good in relation to the other 109īs and the A6M5 keep to much energy at highspeed(similar to the HurriIIc).
In hands of a good pilot the 16 was probably one of the best low level dogfighters in WWII, but according to the pilots already the normal winged Spits did need a good pilot cause the very light elevator, the cw Spit did count as even more difficult regarding the usage of the elevator.
Absolut nothing of this i can find in AH. Who wanna know how bad slowspeed handling and difficult stall behaviour feels in AH, should try the Ta152 at slow speed. In Ta152 the aspectratio related high lift dont seems to work, in oposide to the P38. Even with 25% fuel the Ta snap roll extreme from one side to the next at 105mph(engine out, so torque isnt a argument), while the extreme heavy wingloaded(100% fuel) P38L dont snaproll at all and lower the nose at 95mph(no flaps). The Spit16 lower its nose at 70-80mph and if a roll happen, its rather smoth.
Since the Ta152H is one of the few german planes that got rated as very good even by the allied testilots, i will compare it with the P38L and Spit16:
Wingload:
P38L(100% fuel): 260kg/mē
Spit16(100% fuel) : 158kg/mē
Ta152H(25% fuel): 188kg/mē
Wing aspect ratio(one of the best arguments to explain the good P38 behaviour, despite its high wingload and this is a absolut valid argument. The Aspecratio is at least as important as the wingarea, specialy if it comes to slowspeed lift/drag behaviour):
P38: 8,2
Spit cw: 4,59
Ta152H: 8,8
Power off stall speeds in Ah with the above settings:
P38L: 95-100mph(P38 manual say 100mph with a bit less weight, so thats rather ok)
Spit16: 70-80mph (Pilot notes say 95mph @ 3250kg)
Ta152H: 105mph.
If i compare this datas i would say in Ah they did install the airfoil of the Ta152H headover, or they did calculate it with the Spit16īs aspect ratio, while they took the Ta152H aspectratio to calculate the Spit16 lift.
This would explain why hte Ta152H perform the snap roll of a unstable wing-form and why the Spit16 stall rather smooth(at least in this relation).
This incredible high lift also explain the incredible energy management of the 16.
Greetings,
Knegel