How is pitch controlled in a flying wing?

Question

How do delta wing or flying wing aircraft maintain their pitch attitude in the absence of an elevator? I understand that the ailerons on the wings do control the banking/roll, but they are differential in nature. Then how can they help in pitch control? For pitch control, both control surfaces need to deflect in the same direction.

You should look at "elevon" on wikipedia: "When moved in the same direction (up or down) they will cause a pitching force (nose up or nose down) to be applied to the airframe" — Manu H, Jul 22 '15 at 14:25
You already answered: it's enough to move them symmetrically and you get the pitch control. — Gianni Alessandro, Jul 22 '15 at 14:31

Jae Carr · Accepted Answer · 2015-07-22T15:08:11.577

16

You basically have the answer right inside of the question (as was mentioned in the comments). In order to make the plane pitch up and down you have the ailerons move up or down in unison (usually called an elevon at that point, again, as noted in comments.)

Here's a handy diagram to give you some idea of what we're on about:

In the second image the movement of both elevons upwards will pitch the aircraft up as well. And the elevons going in opposite directions, like the last image, will cause the plane to roll (in this case to the left.)

There are more complex maneuvers as well, like pitching and rolling at the same time. These maneuvers are simply managed by differential deflections of the elevons. Meaning, if you want to come up and to the left you could leave the right elevon neutral(ish) and pitch the left elevon upwards. This would push down the left wing, rolling you to the left, and pitch the nose up as well.

edited Jul 22 '15 at 15:08

answered Jul 22 '15 at 14:47

Jae Carr

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Great! Thanks Jay for the wonderful response. Now I know! – Romi Jul 24 '15 at 16:29
@Romi Sweet, make sure you mark it as correct then ;) – Jae Carr Jul 24 '15 at 16:35
Done! Sorry I didn't know there is an option to mark it as correct. First time! Thanks again! – Romi Jul 28 '15 at 02:42

score 2 · Answer 2 · answered Jul 22 '15 at 17:42

The reason an elevator can cause pitch up/down is by providing a force, pushing down/up, on a point aft of the Center of Gravity (CG).

A canard provides pitch up/down by pushing the nose up/down (forward of CG). An elevator provides pitch up/down by pushing the tail down/up (note that pushing the tail DOWN pushes the nose UP).

Are your elevons (combination elevator/aileron) aft of the CG? If so, pushing both of them down will push the tail up and push the nose down.

How is pitch controlled in a flying wing?

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