I assume that the fuselage and tail fin can generate lift when flying sideways with a constant heading and a little pitch up (er, yaw right assuming left wing down) will introduce a vertical component to the thrust.

Is that all there is? What else might be going on?

  • $\begingroup$ @fooot Thanks. it is a duplicate, I'll close. Cheers. $\endgroup$ – Simon Apr 24 '15 at 21:49