SLC wrote:And Gecko: I know your post was some time ago, but I'll reply here. You clearly have an understanding of what's going on, and I agree with what you say. After thinking about it, I don't mean to say that the induced drag component is negligible on the whole (when the wing is attached). However, I do think the most significant reduction in drag when the wing stalls is from the large reduction in pressure drag (due to the loading on the wing being massively decreased). Yes, the induced drag would also decrease due to this reduced loading (the decrease in loading will reduced the upwash which you get as a result of the trailing vortex system), but that component is still relatively small (I'd say 20-25% of the total drag delta). To be honest I've never had think about, let alone work out, the different components that make up the wing drag (hell, overall car Cd is all that really matters).
Dear SLC,
thanks for the reply!
I think we are mostly in agreement then. I will, however, maintain that the only reason that the pressure distribution on a loaded, mostly unstalled, wing does not press downward but rather somewhat in the direction of the flow is due to the induced upwash. Induced drag does manifest itself through the change in the wing pressure distribution, which is the phenomenon you are describing, and the drag due to this pressure distribution should directly correspond to the energy put into the wing upwash. As with many things in fluid dynamics, I believe we are simply describing the same effect from different, equivalent viewpoints.
I will take the debate one step further and state that stalling a part of the multi element wing would never give any reduction of drag in the case of a very wide wing (the 2D case). It is only because of the limited width and the corresponding upwash effects that one can exploit the phenomenon which you correctly described. Agreed?