Mudge wrote:
I asked the troops at The Fighter Collection and received this reply:
"Have never seen on a Lancaster before but my guess is that they were to straighten out the airflow behind the engines to improve the airflow over the ailerons. Seen on other aircraft.
Best Regards, Peter"
Mudge the researcher
Guys,
I gotta go with the reply from Mudge on this one. The reason I say this is because the British have always been fanatics with repect to aerodynamics on large aircraft. Case in point. The BAC-111. If you look the wing there is what they call or rather what I refer to as the "Potatoe Chip"....is is about 1/3 of the way outboard of the fuselage and it improves direction airflow over the wings and allows a smoother intake for the tail mounted engines. The DC9-10 is simliar....and I beleive neither has Leading Edge slats for increased lift on take-off and landing. The Boeing 757 also has similar vortex generators on the upper surface of the wing.
Additionally, if you look the placement of the strips with respect to what rivet patterns I can discern from the photo, they do not appear to be part of any repair or internal strengthening. So this is, what I think at least, and experimental protoype R&D thing of the day techologically speaking.
Just my two cents though,
Paul