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Aviation History
1950
1950 - 0289.PDF
1950 193 torque tubes, flap actuation being derived from a pair of Dowty hydraulic jacks mounted one in each stub wing and supplied from a common source. Attachment of the outer wing panels to the stub wings is made at the main spar with high-tensile-steel multiple bolts uniting the fork-and-lug-jointed booms. The main spar booms of the wing proper are unusual in being machined from extruded angle-section steel members. These run outboard a distance of 3ft 7m from the joint, whilst progressively tapering in sectional dimensions, and at their extremities are supplemented by fish-plates which provide doubling reinforcement for transition to the heavy- gauge pressed-channel member which forms the main spar for the remainder of the span. As may be seen from the illustrations, this transitional point in the main spar structure HAWKER P. 1052One Rolls-Royce Nene 2 Turbojet Span ... ... 31ft 6inLength 37ft 9.5in Height 10ft I inWheelbue 12ft 9in Trmck 7ft ll.5in Win* are*, gross ... ... 258 sq ftAspect ratio 3.84 Standard mean chord 8ft 2.Sin T/c ratio 10 per cent.Dihedral I deg 45 min Incidence _ 0 deg 30 minSweep-back, lefding edge 40 deg at quarter chord 35 dectrailing edge 15 deg 30 min Tailplane span lift 3inTailptane and elevator area, gross 36.5 sq ft Tailplane incidence, range 5 degnominal setting + I deg fin and rudder area, gross 21.5 sq ft
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