Wing performance issue
Wing performance issue
(OP)
Hi guys,
I need to assess the performance of a wing when increasing the camber of the grid sections, getting at the end a more cambered tip. I do not take into account any high-lift devices (e.g., aileon) but probably the performance I seek is with respect to a conventional wing. Does anyone have any idea or papers on the subject?
regards,
J
I need to assess the performance of a wing when increasing the camber of the grid sections, getting at the end a more cambered tip. I do not take into account any high-lift devices (e.g., aileon) but probably the performance I seek is with respect to a conventional wing. Does anyone have any idea or papers on the subject?
regards,
J





RE: Wing performance issue
Check with Missisippi state university, Dr gus Raspet carried out several experiments on this subject.
He also built an aircraft that changed the camber of the wing with internal cranks. I believe it was called the Marvel.
B.E.
RE: Wing performance issue