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View Full Version : Delta wing and Canard vs 'Conventional'


stilton
4th Nov 2016, 04:18
I find it interesting that while all contemporary US fighters have stuck with
a conventional wing and horizontal stabilizer layout modern European aircraft have gone with the delta wing with canard.


Typhoon / Gripen / Rafale all use this layout and there seem to be great advantages in terms of maneuverability, weapons and fuel capacity.
Curious as to why there's such a philosophical difference in design, is it maneuver driven or is there any relationship to stealth requirements.


Is there something intrinsically 'unstealthy' about a canard / delta layout that US designers would steer away from , or is it a case of staying with what they are most comfortable ?

msbbarratt
4th Nov 2016, 06:05
The canards are useful for improved manoeuvrability at high angles of attacks as they're not masked from clean airflow by the wing itself at such attitudes.

I don't see that a canard is necessarily unstealthy, it depends what you make it out of.

Delta wings were considered by some designers in the old days to be a bad idea. Maybe that opinion stuck amongst the American design community. There's pros and cons to any wing design, and there's no real killer reason to choose a delta or something else. But I guess if one chooses a delta wing, canards make a lot of sense too.

57mm
4th Nov 2016, 06:36
Pedant mode on: if moveable, they are foreplanes, not canards: pedant mode off: sorry peeps.

Trim Stab
4th Nov 2016, 07:19
I've always assumed that it is because the US has a half-generation or so lead in fly-by-wire, stability control and aerodynamics, which allows them to get the required performance without foreplanes (which are likely to add cost, complexity, weight, radar profile, and drag).

Basil
4th Nov 2016, 07:34
Pedant mode on: if moveable, they are foreplanes, not canards: pedant mode off: sorry peeps.
So, to call it a 'canard' is, in fact, a canard.

Hat, coat, door . .

andytug
4th Nov 2016, 08:26
So, to call it a 'canard' is, in fact, a canard.

Hat, coat, door . .

At least it's not "Fore canard".

(works best in Scouse accent)

JonnyT1978
4th Nov 2016, 08:44
Wasn't the Viggen an inherently stable aircraft despite its' early canard-style (albeit not all-moving) layout?

One of the criticisms levelled at earlier 'pure' delta aircraft (such as the Mirage III/5) was that they bled too much airspeed in tight turns. Not sure how well (if at all) this was overcome with the later Mirage 2000...

On the other hand, GD/LM claimed that the double-delta 'cranked arrow' layout of the research only F-16XL (or F-16E) made canards unnecessary. Always wondered about this claim!

I think the 'secret' to instability (and thus turning performance) is loading the c.g. as far aft as possible. The 'normal' F-16 is a good example of this in a conventional layout. Canards just provide an efficient way of controlling the pitch-up tendency.

Pontius Navigator
4th Nov 2016, 09:31
I think a lot is to do with design fashions. Remember also the Russians used canard etc on the SU22 (IIRC) and Concordski etc. Swing wing was fashionable before that, AFVG, Fitter etc.

Before that tailless deltas, B58, FD2 etc.

So you might argue that the US are ahead of the game with stealth tail less coming in.

pasta
4th Nov 2016, 10:28
If it looks like a canard, and quacks like a canard...

I'll join the queue for the cloakroom.

megan
4th Nov 2016, 11:26
if moveable, they are foreplanes, not canardsSo why do the designers/manufacturers of foreplane equipped aircraft call them canards?

Davef68
4th Nov 2016, 11:46
Technological generations - Rafale, Typhoon, Gripen are all in the generational gap between the F15/F16/F18 and the F-22/F35.

melmothtw
4th Nov 2016, 12:14
Pedant mode on: if moveable, they are foreplanes, not canards: pedant mode off: sorry peeps.

So why 'Euro-canard' and not 'Euro-foreplane'?

Edit: Ahh, see megan asked the same thing

57mm
4th Nov 2016, 13:36
Well, I can't answer for the makers or engineers, but I assure you that to the aircrew, they are foreplanes.

Incidentally, the canards on the Viggen are "flapped", for STOL performance. Watch one on YouTube.

DITYIWAHP
4th Nov 2016, 14:21
Everything in Typhoon is 'modern' so all of the terms for the systems and components are 'modern' as well, just so you don't forget.

I have read some new (< 10 yrs old) publications that refer to these before-wing control surfaces as foreplanes, but I have read many other (more classical) aerodynamic reference documents that refer to them as canards. Some even refer to the wing-foreplane combination as a canard configuration... This appears to be a European creation - modern US reference literature has yet to catch up.

It's a bit like saying that fuel quantity must be measured in Kg.

Rhino power
4th Nov 2016, 15:50
Another term for canards of the all-moving variety, a la Typhoon/Gripen/Rafale, is 'canard foreplane', which does seem the best description, imho...

-RP

Willard Whyte
4th Nov 2016, 16:41
Pedant mode on: if moveable, they are foreplanes, not canards: pedant mode off:

Which pretty much guarantees we'll keep calling them canards. (See comments regarding drone vs. 'uav' etc).

Treble one
4th Nov 2016, 18:27
Am I right in thinking that at high AoA canards/foreplanes are much better than a conventional tail as the delta wing can obstruct airflow over the tail inducing some very nasty problems (thinking Javelin?)-or have I got that all wrong?

Fatnfast
4th Nov 2016, 19:43
I got told by a tame aerodynamics chap at work, that having foreplanes enabled far better maneuverability than a pure delta, and that as the foreplanes produce a lifting force rather than a downforce (as with a conventional tail); then you could get away with a smaller wing and still have good turning performance.

EAP86
4th Nov 2016, 22:21
Conventional delta wings can struggle with control saturation at high incidence. The flaperons run out of authority in pitch and roll. Foreplanes enable the flaperons to operate around their mid position so you don't run out of control authority at the extremes. They also help with trimming across the Mach range. Foreplane/deltas can also achieve performance targets with lower overall masses, helpful if you believe there's a correlation between mass and costs.

Having said that, PN might be closer to the truth i.e. fashion may have a lot to do with it. Quite a few years ago part way through Typhoon development, an aerodynamicist suggested that a foreplane delta probably wasn't the best concept based on the latest thinking. He mentioned a foreplane delta with a tail was the way to go. If you believe the SU30's odder manoeuvres are the future of air combat, he might be right.

EAP

Rhino power
4th Nov 2016, 23:32
If you believe the SU22's odder manoeuvres are the future of air combat, he might be right.

EAP

The SU-22 is a swing-wing, (mostly) bomber, perhaps you mean the SU-30MKI?

-RP

megan
5th Nov 2016, 01:18
In the literature the terms canard and fore plane are used interchangeably.

Whether a canard offers advantages comes down to the usual engineering and aerodynamic trade offs. With a canard the wing can not reach its max CL and be allowed to stall before canard stall, though I guess that may be obviated with an all moving canard as on the Eurofighter.

Arm out the window
5th Nov 2016, 05:12
One interesting development in foreplane technology was experiments with longitudinal positioning, i.e. varying the fuselage station and centre of gravity to get the best compromise of strength vs. manoeuvrability.

Starting from a significantly rearward position, aerodynamicists tried incrementally moving the foreplane forward on a specially built test vehicle, which initially gave improvements which peaked, then started to decline.

At this point, the testing scientists declared "This is too far canard."

riff_raff
6th Nov 2016, 01:50
Don't any of you recall the mach 3+ XB-70? It had delta wings with outer sections that could be rotated down in flight. And it had huge canards with trailing edge flaps. All way back in the early 60's.

http://www.flyinginthespirit.cuttys.net/wp-content/uploads/2015/12/xb-70-landing.jpg

Brian Abraham
6th Nov 2016, 02:03
it had huge canards with trailing edge flaps. All way back in the early 60's.So did the Wright Brothers, all the way back in 1903, plus theirs was all moving, just like the Typhoon. Talk about advancement.

57mm
6th Nov 2016, 13:20
Ah, so it was a foreplane then.....

megan
6th Nov 2016, 23:06
Ah, so it was a foreplane thenNot even. The Brothers actually called it the "front rudder". Which means the Typhoon has a front rudder. :p

Arm out the window
7th Nov 2016, 01:30
An awkward term, a bit like 'front bottom'!