In 1947, the G-72 was modified for ducted-wing testing as the "'G-81 "', it was fitted with slotted flaps to induce slow flight.
42.
These included stretching the fuselage and increased maximum takeoff, maximum landing, and maximum zero-fuel weights, with the wing modified to incorporate double-slotted flaps and drooped leading edges and tip tanks.
43.
The Ibex was designed by Hall to investigate the reduced wetted area of the pod and boom configuration, hands off spiral stability of a gull wing, and the low speed performance of wide NACA slotted flaps.
44.
The Bf 163 followed closely the formula established by the Fi 156 in being a high-wing braced monoplane with a metal structure, automatic leading edge wing slots, double slotted flaps, and an exceptionally tall undercarriage.
45.
Test flights confirmed wind tunnel tests that revealed a lack of flaps proved to be unsatisfactory during flight testing, but all three prototypes and the first 14 production aircraft were built with them before they were replaced with a single-slotted flap.
46.
The maximum lift that can be achieved before stall, in terms of the lift coefficient, is generally less than 2.0 for single-element airfoils and can be more than 3.0 for airfoils with high-lift slotted flaps deployed.
47.
In conjunction with the leading-edge slats, 74 % of the trailing edge incorporates high-lift slotted flaps, which together with interrupter blades atop each wing when roll control is lost at very low airspeed, allows for a tight turning radius.
48.
Despite its numbering sequence it was actually developed after the Falcon 20, and although it is sometimes considered as a scaled-down version of that aircraft, it was totally redesigned with a non-circular fuselage, a new wing with slotted flaps, a split passenger door and many simplified circuits compared to the Falcon 20.
49.
Amongst the differences between the VC5 and the VC7 were a larger 12 ft 6 in ( 3.81 m ) fuselage with six-abreast seating for 131 passengers, the wings having been relocated to a low-mounted position, the addition of slotted flaps, and the overall size of the wing being considerably larger.
50.
Other STOL features included a dorsal and two ventral fins on the rear fuselage, double-slotted flaps and extended ailerons, a new radome, a tailhook for landing aboard an aircraft carrier, and Combat Talon avionics, including a Terrain Following / Terrain Avoidance radar, a defensive countermeasures suite, and a Doppler radar / GPS tie-in to the aircraft's inertial navigation system.
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