The elliptical wing of the Spitfire allowed a thick centre section to accommodate the undercarriage, and 4 x .303" machineguns. The wing had the advantage of its stalling characteristic, in that it stalled on the inboard end first, and the tip last which meant that the aircraft remained in control right to the last instant , this was important in tight turns in combat, the ME 109 if forced into tight turns in combat with the Spitfire would go into a high speed stall, and flick out, I believe that the ME 109 could be difficult to handle in these situations.
The Spitfire Vb with the cut of wing tips gave better handling at low altitude, and faster rate of roll below 20,000ft. These aircraft had bomb racks for either two 250lb, or one 500lb bombs, and with there canon armament were used for ground attack. they had about 4ft removed from the wing span. The ones with the extended wing tips were fitted with pressure cabins for use at extreme altitude, service ceiling of 42,000ft Compared to 36,000ft for a similar aircraft with standard wing span.
The Mustang got around the drag problem in a way that was not available to Mitchell in 1936, North American used a laminar flow aerofoil, and as long as the aircraft was clean(no bugs or mud), it worked well.
Ian S C
Edited By Ian S C on 07/03/2016 10:40:35