Dave Rogers
Bandaged ice that stampedes inexpensively through
Since the angle of attack is relative to the velocity vector, the negative AoA would place the veolcity vector at roughly 60 degrees relative to the ground. This would be in favor of less plowing but still can't account for the wings being on the wrong side. The AoA at -20 degrees should be providing negative lift carrying the wings further towards the far side of the crater.
What you seem to be missing is that the central crater, where the fuselage hit, appears to be significantly larger than the fuselage. If the aircraft was travelling at a negative angle of attack, the nose would have hit the ground at a point further from the tail imprint than the points at which the bases of the wings first hit. There would be some enlargement of the crater back towards the point of impact of the wings, but the deceleration would also generate a shockwave travelling towards the tail of the aircraft which might cause some disintegration of the rear fuselage. This would mean that the fuselage crater was caused primarily by the impact of the front half of the plane, and the angle of attack would cause this to be elongated in the direction away from the tail impact - in other words, exactly what is seen. I'm not sure how clear that is, but I can visualise the geometry and it seems reasonable to me.
I doubt whether there would be enough time for the negative lift to affect the trajectory of the wings from the time the fuselage broke up to the time they impacted the ground. In any case, the wings wouldn't have to "go through the fuselage" to achieve the effect you're claiming - they wings are, of course, on either side of the fuselage, so they'd just have to separate and follow a slightly different trajectory.
Dave