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The subtle and graceful external shape of Concorde hides a great many advanced engineering features. The wing is a masterpiece of aerodynamic shaping. The slender delta shape with an ogival (curved) leading edge was only arrived at after a huge amount of wind tunnel testing and reaches optimum efficiency at around Mach 2.2. Most of the fuel is stored in the wings, where it acts as a heat sink for the wing skin during prolonged supersonic flight. Fuel is also used to control the aircraft centre of gravity, to counter-act the rearward shift in the centre of lift as the aircraft goes supersonic. Fuel is pumped into trim tanks in the rear fuselage during acceleration and forward again during deceleration to subsonic speed. Computer controlled variable-area air intakes ensure that each engine receives an optimum air flow under all flight conditions. The nose of the aircraft can be hinged down 17.5 degrees to improve the view of the pilot while landing or taking-off, although in practice only 12.5 degrees is normally used.