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Wibault 2

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As the military description BN.2 indicates, the Wib 2 was designed as a two-seat night bomber, but the designer had hopes of a passenger carrying derivative. As it was structurally an all-metal aircraft it had, by the standards of the times, a low structural weight and, as a consequence, a high
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useful load of 1,406 kg (3,100 lb) making the suggested capacity of thirteen passengers plausible. In addition to its metal construction, contemporaries noted other unusual design features, in particular the position of the wings well back along the
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and over a greater longitudinal distance than usual, rather than along the span. The pilot sat quite close to the tail with the gunner (in the bomber version) in a separate, gun mounting equipped cockpit immediately behind him. Its span was large for a
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The Wib 2 flew for the first time on 29 October 1921 but only one, in bomber configuration, was built.
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speculated the idea being to distribute the passenger (or bomb) load symmetrically about the
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projected out on either side of the cowling. The undercarriage was of the fixed
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201 km/h (125 mph, 109 kn) at 1,980 m (6,500 ft)
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supported the upper wing above the fuselage. The wings had thick, high
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mounted on top. Its vertical tail was low and broad, with a curved
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The wings of the Wib 2 were rectangular in plan and mounted without
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sheet; the ribs were formed from cross-braced metal tubes.
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and its upper wing had a shorter span than the lower.
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in the early 1920s. It was intended as a heavy night
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Small 195:Ailerons 167:dihedral 141:fuselage 675:Wib 368 670:Wib 367 665:Wib 366 660:Wib 365 655:Wib 362 645:Wib 313 620:Wib 260 615:Wib 240 610:Wib 220 605:Wib 210 580:Wib 123 491:Wibault 302:Height: 290:Length: 230:cowling 163:stagger 120:biplane 555:Wib 10 540:Wib 74 535:Wib 73 530:Wib 72 525:Wib 71 448:Flight 357:Range: 218:rudder 216:; the 146:Flight 128:bomber 124:France 61:France 550:Wib 9 520:Wib 7 515:Wib 3 510:Wib 2 505:Wib 1 278:Crew: 187:spars 112:Wib 2 44:Role 422:2013 328:1 × 106:The 165:or 114:or 718:: 445:. 430:^ 399:^ 143:, 110:, 100:1 482:e 475:t 468:v 424:. 384:: 20:)

Index

Wibault Wib.2

France
Pierre Lavasseur
Michel Wibault
biplane
France
bomber
fuselage
Flight
centre of pressure
biplane with only a single set of struts
stagger
dihedral
interplane struts
flying and landing wires
Cabane struts
lift coefficient
spars
Duralumin
Ailerons
fabric covered
tailplane
elevators
leading edge
rudder
aerodynamically balanced
Renault 12 M
cowling
propeller

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