Decalage: The difference in incidence between the upper and lower wings of a biplane.
Lots of designers have some decalage on their biplane designs. The reasons given are usually pretty feeble to my way of thinking, especially at model sizes.
Usually, biplanes which are only equipped with ailerons on the lower wing have the top wing set at a higher angle than the lower wing. The reason given is that the top wing will stall first (true) so leaving the lower wing unstalled and therefore maintaining aileron control, as (theoretically) the lower wing is still flying.
In reality, when the top wing stalls and stops producing lift, the entire weight of the aircraft is suddenly transfered to the lower wing, which, as you would guess, stalls instantly on being burdened with all this extra weight.
Personally, all my bipes have no decalage, and others that have come into my possesion, have flown better for having the decalage taken off. One in particular, had some three degrees plus of decalage and was a very pitch sensitive machine with unpredictable stalling habits. On removing the decalage the machine was transformed and became a sweet handling aircraft.
So why do designers persist in using it?
Lots of designers have some decalage on their biplane designs. The reasons given are usually pretty feeble to my way of thinking, especially at model sizes.
Usually, biplanes which are only equipped with ailerons on the lower wing have the top wing set at a higher angle than the lower wing. The reason given is that the top wing will stall first (true) so leaving the lower wing unstalled and therefore maintaining aileron control, as (theoretically) the lower wing is still flying.
In reality, when the top wing stalls and stops producing lift, the entire weight of the aircraft is suddenly transfered to the lower wing, which, as you would guess, stalls instantly on being burdened with all this extra weight.
Personally, all my bipes have no decalage, and others that have come into my possesion, have flown better for having the decalage taken off. One in particular, had some three degrees plus of decalage and was a very pitch sensitive machine with unpredictable stalling habits. On removing the decalage the machine was transformed and became a sweet handling aircraft.
So why do designers persist in using it?
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