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In article , Guy Alcala 
		
	
		
		
		
		
		
	
		 
		
	
	
	writes 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 Some penny-pinching accountant at work perhaps? I was always mystified by the fact that the Spitfire didn't get full wheel-well covers until late in the war - they went to all that trouble gluing split peas all over the wing to optimise the placement of flush and round headed rivets and missed out on some thing that seems even more obvious (unless the drag from the wheel well really was inconsequential up to speeds of 400 mph or so - but that seems a bit counter instinctive). Cheers, Dave -- Dave Eadsforth  | 
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