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NWSRG
13th Nov 2004, 16:30
Folks,

Do Boeing and Airbus have significantly different wing design philosophies?

To me, Airbus flaps seem to be smaller than their Boeing counterparts, and seem to extend less.

Boeings tend to have higher cruising speeds.

Are Airbus wings optimised for broader performance across a wider speed range (thus requiring less flap to land), with Boeing tending to choose a better high-speed design and fitting bigger flaps for low-speed control?

ukeng
13th Nov 2004, 19:30
http://www.cartoonstock.com/lowres/cga0275l.jpg

:)

A333
13th Nov 2004, 21:27
I have read somewhere that the Airbus A330/340 wing is designed softer and flexier to abosorb turbulence better. Is this true?

NWSRG
14th Nov 2004, 12:40
Promise...not trying to open a can of worms!

Only asking if an observation is correct!

...and not suggesting which approach is "better"!!

minibus3
14th Nov 2004, 12:44
I believe that, for an unknown reason, Airbus wings produce less vorticies, thus less induced drag.

My contribution.

Cheers

SOON2B
14th Nov 2004, 18:33
I believe vorticy size is a function of speed. If we fly our Boeing slower it acts like a bus?? OK, the can of worms is open.:ouch:

747FOCAL
14th Nov 2004, 19:21
Each company has its better wings for comperable aircraft vs. the other. Sometimes the manufacturer gets it right and sometimes things just don't turn out exactly the way you thought they would.

But one of the two is known, as SOON2B points out, for Being "low and slow". :E

minibus3
14th Nov 2004, 20:46
I agree; but what I meant was that for a given set of flight conditions(speed included), Airbus wings produce less vortices than Boeing wings.

swh
15th Nov 2004, 02:04
I was of the understanding that Airbus does not do any wing design, its sub contracted to British Aerospace.

GearDoor
15th Nov 2004, 03:09
Doesn't the 777 have a single-segment flap?

Volume
15th Nov 2004, 05:55
When Airbus introduced the A310 (http://www.airbus.com/pdf/customer/fast05/wing.pdf), it was the aerodynamically most advanced wing in transport aircraft design, obviously much better than any existing Boeing design at that time. For modern Boeing design, there is not much difference to modern Airbus design, both are at comparable level of aerodynamic performance.
Anyway both companies follow a sligtly different optimisation idea, Boeing wings have a little more sweep. This improves high speed performance by reducing transsonic drag. Therefore Boeing aircraft cruise a little faster. On the other hand wingsweep is bad for high lift performance, especially the outer wing is not able to work at high CL. To compensate for this Boeing wings have to use more sophisticated trailing edge devices like multiple slotted flaps.

If you compare the B777 (http://www.airliners.net/open.file?id=711576&WxsIERv=Qm9laW5nIDc3Ny0zMTI%3D&WdsYXMg=U2luZ2Fwb3JlIEFpcmxpbmVz&QtODMg=QmFuZ2tvayAtIEludGVybmF0aW9uYWwgKERvbiBNdWFuZykgKEJLS yAvIFZUQkQp&ERDLTkt=VGhhaWxhbmQ%3D&ktODMp=T2N0b2JlciAzMSwgMjAwNA%3D%3D&BP=1&WNEb25u=UG9vd2luIEJ1bnlhdmVqY2hld2lu&xsIERvdWdsY=OVYtU1lI&MgTUQtODMgKE=&YXMgTUQtODMgKERD=MTM3&NEb25uZWxs=MjAwNC0xMS0xMw%3D%3D&ODJ9dvCE=&O89Dcjdg=MzIzMTcvNDIw&static=yes&size=L) wing flaps to the A330 (http://www.airliners.net/open.file?id=712096&WxsIERv=QWlyYnVzIEEzMzAtMjQz&WdsYXMg=TGl2aW5nc3Rvbg%3D%3D&QtODMg=TGlzYm9uICgtIFBvcnRlbGEgZGUgU2FjYXZlbSkgKExJUyAvIExQU FQp&ERDLTkt=UG9ydHVnYWw%3D&ktODMp=T2N0b2JlciAzLCAyMDA0&BP=1&WNEb25u=S3J6eXN6dG9mIFNrb3dyb25za2kgW2Vwd2Ffc3BvdHRlcnNd&xsIERvdWdsY=SS1MSVZO&MgTUQtODMgKE=&YXMgTUQtODMgKERD=MjM%3D&NEb25uZWxs=MjAwNC0xMS0xNQ%3D%3D&ODJ9dvCE=&O89Dcjdg=NTk3&static=yes&size=L) design, you see the large gap between inner and outer flaps at the engine position for the Boeing, while the Airbus flap is continous. To have the same overall high lift performance, the flaps with ´engine window´ need to have better performance than the continous, therefore they have to be slotted.

PAXboy
15th Nov 2004, 13:51
As a pax, I have learnt from flight crew that Airbus wings were designed for fuel economy. They go slower but are smoother and, for the distance, the amount of fuel saved is significant.

On a short or medium haul, the time diff for an Airbus wing is negligible. On the long haul, it becomes noticeable but not significant. For example. LHR ~ JNB: This non-stop sector of (avergae) some 10.5 hours, is shown with 30 minutes extra for the A340 against a B747. I gather that the time is less than that but 30 mins is easier on the schedule for pax to understand.

So, from a pax point of view, it's irrelevant. From the human point of view, when I hear people boasting that their toy goes X knots faster than another, I think: Bunch of babies. :rolleyes:

--------------------
"I tell you, we are here on Earth to fart around, and don't let anybody tell you any different." Kurt Vonnegut, Jr.

TURIN
15th Nov 2004, 18:01
There are no vortex generators on Airbus wings.:E

Self Loading Freight
16th Nov 2004, 15:41
I'm just glad there is a difference. As everyone gets better and better computer modelling, runs the same routes burning the same fuel with interchangeable engines, I wouldn't be surprised if it all ends up at the same ultra-optimised geometry. Dull or what?

R