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#11
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Dave Eadsforth wrote:
snip To enlarge on my 'thick wing section' description, and working from memory of a book read long ago (which can be fatal), I recall that Davis conceived of a wing section that was based on a mathematically deformed circle, which he believed would give a more laminar flow. The thicker, 'teardrop-shaped' aerofoil section that resulted was also very useful structurally, given that he wanted to combine it with a high aspect ratio wing. Of course, any wing section inboard of the engines was going to have its airflow messed up considerably by a few minor essentials; like engine nacelles and de-icing boots etc etc, but the wing outboard of the engines may have performed as Davis believed it should during cruise. snip He was quite irritated that Consolidated didn't provide full covers for the main gear wheel wells, as he felt that defeated much of the drag reduction. Guy |
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