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Old 12 May 2004, 11:56 AM   #1 (permalink)
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Probably a very silly question but ...

... why were wings staggered forward or backward?

When building a biplane the easiest way would be to place them like on a Spad VII.

Were staggered wings just a way to improve the view of the crew or was there a general technical concept behind the very common forward staggered wings (S.E.5) and the less often seen backward staggered wings (Sopwith Dolphin)?


Thank you in advance for your help.
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Old 12 May 2004, 01:32 PM   #2 (permalink)
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Depending on how it is done staggering wings, either forward or backward can accomplish of number of desireable flight characteristics in an aircraft in addition to better visibility - it can reduce interference drag and reduce corresponding wingtip lift loss, it can improve center of gravity, and reduce stall speed.
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Old 12 May 2004, 01:56 PM   #3 (permalink)
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Volker_Nemsch Posted: May 12 2004, 10:56 AM
Quote:
Probably a very silly question but ...

... why were wings staggered forward or backward?
I dunno why, but it sure looks pretty on a Beechcraft.
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Old 12 May 2004, 06:50 PM   #4 (permalink)
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A wing builds a low pressure area above the thickest point, which is how planes fly. This low extends up and back for a considerable ways depending on the speed, among other things. If there's another wing in this area, the low actually pulls down on the top wing, losing net lift. By staggering the wings, the top one is moved out of the peak low pressure area.
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Old 12 May 2004, 07:01 PM   #5 (permalink)
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Is this related?

Lower wings offset from the fuselage such as Bristol F2s and Pfalz D.XV?

Have never understood that and seen it as complicated - at least for the rigger.

Anyone?
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Old 13 May 2004, 01:08 AM   #6 (permalink)
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I had the same idea while looking through my picture archive.

The Dorand AR.2 below is an interesting example for this ...
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Old 13 May 2004, 05:09 AM   #7 (permalink)
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Backward stagger seems to be a dead end with more drawbacks than benefits, given that it was seldom used. The most notorious case was the Airco DH5, where the attempt was to keep the great visibility of the DH2 in a tractor biplane, and the craft resulted a failure, I suspect much of the blame was due to the back stagger wing.

Regarding the Beechcraft, the stagger wing was used by these reasons

"The seldom used stagger wing configuration has the bottom wing forward of the top wing, and at a higher angle of attack. This ensures that the bottom wing always stalls first. When this happens, the sudden loss of lift drops the nose, which prevents the top wing from stalling. In other words, only the bottom wing stalls, and then you are still flying a lightly-loaded high wing airplane."
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Old 13 May 2004, 05:29 AM   #8 (permalink)
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Originally posted by R Pope@May 13 2004, 01:50 AM
[b]If there's another wing in this area, the low actually pulls down on the top wing, losing net lift. By staggering the wings, the top one is moved out of the peak low pressure area.
Suddenly the odd appearance of the Nieuport Triplane begins to make sense...

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Old 13 May 2004, 05:30 AM   #9 (permalink)
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Regarding the fuselage "suspended" between" the wings

Here's my conjectures

1) a way of getting a little more wing surface thereby increasing lift
2) ease of fabrication,
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Old 13 May 2004, 05:50 AM   #10 (permalink)
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Me too.

Ease of wing fabrication but more for a rigger.

Is that enough?

There must be some "value" engineers theorized.

The Nieuport Triplane makes me think these guys weren't so "crackpot" after all, given the above description of the Staggerwing flight characteristics.

Is this all self-evident to some pilots and all aeronautical engineers and why little comment attends these things?

I'm ignorant.
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