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I was watching videos of F-35B taking off and landing vertically on ships when I realized that when transitioning from horizontal to vertical flight mode (I don't know the exact vocabulary to describe that), the horizontal elevator moves to "stick pushed full forward" position. The elevator is also put in that unusual position when transitioning from taxiing to a vertical takeoff. I know that the elevator position is not significant in vertical flight as attitude is controlled via non-aerodynamics means. Thus I wonder why this control surface is then put in that position for that flight phase instead of staying in its previous position or in a more neutral position.

I'm even more confused as this behaviors doesn't seems to be reproduced on other VTOL fighters such as the AV-8B or the Yak-141.

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In this video you can see it better I think:

F35B in hover in side view

I drew on a screenshot of the video from the side where you can see the air moving under the aircraft.

Compare this to the Fig. 1 in the paper linked by "Anonymous Person" here in the comment section of your question: http://ltces.dem.ist.utl.pt/lxlaser/lxlaser2016/finalworks2016/papers/03.2_3_366paper.pdf

As you can see angling the tailerons down significantly widens the gap between the leading edge of the tailerons and the trailing edge of the wings which allows air to be pulled along with the exhaust gases (drawn in blue). The paper calls this "entrainment".

F35B in hover from read-side view

Again I drew on another screenshot of the video and illustrated possible air currents that can freely move around the airframe: aft of the exhaust duct and to the left and right of the vertical stabilizers. As you can see the flaps are also extended which helps guide the air around the wings. There probably is a similar airflow around the front section of the fuselage where the wings are not blocking the flow and the fan is pushing the air down.

In a vertical descent or climb the tailerons also create less aerodynamic drag in this configuration than in a leveled attitude so the pitch inducing effects due to the large surfaces at the rear are reduced.

It could also be beneficial to angle the tailerons trailing edge down for a vertical landing or a short takeoff to increase the lift at the rear end by blocking the escape path for air trapped under the rear end of the aircraft. Essentially preventing the cushion of air to escape at least when in ground effect.

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Vertical flight needs the big panel behind the canopy open, to admit air to the LiftFan® that it otherwise covers. While that's open, in the transition to horizontal forward flight it would pitch the nose up. The deflected elevators might compensate for that, although the downward-vectored thrust at the rear of the airplane compensates more effectively during slow forward flight (as shown in the video in Anonymous Person's comment.)

The AV-8B lacks such a speed-brake-like protrusion, so it needs no elevator deflection to compensate.

The Yak-141 has what looks like a smaller panel. Photos of it hovering show no elevator deflection, but the far-aft flaps are strongly deflected, perhaps for the same purpose.

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  • $\begingroup$ I think you are wrong as in this video we can clearly see that the liftfan doors opens several seconds before elevators deflection, while the speed is the same (the aircraft is not moving at all and on the ground) $\endgroup$
    – Manu H
    Apr 28 '20 at 6:58
  • $\begingroup$ This is probably not the case, because in this video (youtube.com/watch?v=vsKwBzt7rDY), at the 2:12 mark, you can see the F-35 flying around, pretty fast, with the liftfan cover fully open, without much elevator deflection. $\endgroup$ Apr 28 '20 at 16:13
  • $\begingroup$ @AnonymousPerson nice video! it clearly shows that when the liftfan doors are open, the elevator deflection is more pronounced at low speed (e.i. when aerodynamic controls are not needed). $\endgroup$
    – Manu H
    Apr 30 '20 at 7:12

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