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On its first flight early in 1923, the Rateau turbo-supercharger was not fitted, its development having been interrupted by repeated failures caused by the difficulty of producing suitable high temperature resistant alloys. As a result, it was cancelled by the (S.T.Aé). The Wib 3 continued its flight
122:(S.T.Aé, Technical Department of Aeronautics) for a high altitude fighter. This was required to have a top speed of 240 km/h (149 mph) at 7,000 metres (23,000 ft) and a
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mounted at the roots of the interplane struts. The axle was enclosed within an aerofoil shaped fairing which added 1.50 m (16.15 sq ft) to the wing area.
710:
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from the 1920s, designed for high altitude operations. Its development was abandoned after repeated materials failure in its
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to about half span. The wing section to half span was moderately thick but thinned outboard, giving an overall maximum
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was aluminium skinned from its nose to the cockpit; aft, it was fabric covered. Its wire braced, almost triangular
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of 8,500 metres (27,900 ft); to achieve this performance at altitude, the specification called for a
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testing until the autumn of 1923, after which the high altitude specification was withdrawn.
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149:, ensured the pilot a good all round view. The wing was straight edged with constant
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or fighter, 1 indicating single seat) was
Wibault's response to a call from the
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157:. It was braced to the lower fuselage on each side with a pair of parallel,
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It was an all-metal aircraft in the contemporary sense, with a structure of
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160 W/kg (0.097 hp/lb) from Flight, who give a power loading of 10.3 lb/hp
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850 km (530 mi, 460 nmi) at 5,044 m (16,550 ft)
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supercharger maintained power up to 4,600 metres (15,000 ft). The
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Bruner, Georges (1977). "Fighters a la
Francaise, Part One".
486:. Godalming, UK: Salamander Books. p. 175 (D.8), 595–6.
224:
161:
223:, with mainwheels on a rigid axle supported by a pair of V-
458:. Vol. XV, no. 22. 31 May 1923. pp. 289–90.
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25:
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215:, the inner ends cropped to allow movement of the broad
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241 km/h (150 mph, 130 kn) at sea level
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482:Green, William; Swanborough, Gordon (1994).
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536:"L'avion de Chasse Monoplan Wibault 3C1"
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141:. A parasol wing, with a cut-out in the
377:53 kg/m (10.8 lb/sq ft)
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371:7,000 m (23,000 ft) service
296:25.00 m (269.1 sq ft)
171:The Wib 3 was powered by a 224
284:11.72 m (38 ft 5 in)
278:8.20 m (26 ft 11 in)
195:on each side of the fully enclosed
120:Service Technique de l'Aéronautique
114:The Wib 3, or Wib 3 C.1 (the C for
13:
528:
450:"A New French All-metal Aeroplane"
290:3.04 m (10 ft 0 in)
14:
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542:(in French): 138–141. 15 May 1923
242:
258:Green & Swanborough pp.595-6
24:
833:Single-engined tractor aircraft
504:
585:Aircraft designed or built by
409:, firing through propeller arc
402:2×7.7 mm (0.303 in)
153:and was fitted with long span
1:
823:1920s French fighter aircraft
484:The Complete Book of Fighters
418:
308:1,420 kg (3,131 lb)
7:
332:, 220 kW (300 hp)
302:994 kg (2,191 lb)
10:
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221:conventional undercarriage
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314:227 kg (500 lb)
23:
18:
251:Wibault 3 C.1 three view
219:. The Wib 3 had a fixed
263:General characteristics
252:
239:
110:Design and development
818:Parasol-wing aircraft
787:Vickers Wibault Scout
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237:
183:upright water-cooled
407:Vickers machine guns
696:Wibault 170 Tornade
253:
240:
166:lift to drag ratio
805:
804:
322:Hispano-Suiza 8Fb
181:Hispano-Suiza 8Fb
92:Wibault Wib 3 C.1
84:
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62:Pierre Levasseur
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828:Wibault aircraft
641:Wibault 8 Simoun
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100:fighter aircraft
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41:Type of aircraft
38:fighter aircraft
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797:Vickers Viastra
780:Vickers-Wibault
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686:Wib 125 Sirocco
681:Wib 124 Sirocco
671:Wib 122 Sirocco
666:Wib 121 Sirocco
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529:Further reading
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139:fabric covering
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48:National origin
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513:Air Enthusiast
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351:Maximum speed:
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243:Specifications
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211:carried split
187:engine with a
168:of almost 20.
145:over the open
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71:Michel Wibault
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238:Wibault 3 C.1
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143:trailing edge
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94:was a French
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77:First flight
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59:Manufacturer
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544:. Retrieved
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515:(3): 85–95.
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505:Bibliography
483:
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414:
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404:synchronised
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330:supercharged
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191:cylindrical
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137:but largely
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128:turbocharged
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104:supercharger
96:parasol wing
91:
87:
85:
36:Single seat
540:L'Aérophile
344:Performance
336:Propellers:
318:Powerplant:
812:Categories
419:References
382:Power/mass
363:Endurance:
294:Wing area:
175:(300
98:prototype
19:Wibault 3
746:Wib 360T5
656:Wib 10/II
546:30 August
521:0143-5450
282:Wingspan:
256:Data from
213:elevators
209:tailplane
135:duralumin
88:Wibault 3
80:Q1, 1923
67:Designer
736:Wib 283T
731:Wib 282T
726:Wib 281T
721:Wib 280T
392:Armament
338:2-bladed
205:fuselage
193:radiator
155:ailerons
130:engine.
116:Chasseur
771:Wib 368
766:Wib 367
761:Wib 366
756:Wib 365
751:Wib 362
741:Wib 313
716:Wib 260
711:Wib 240
706:Wib 220
701:Wib 210
676:Wib 123
587:Wibault
288:Height:
276:Length:
197:cowling
189:Lamblin
147:cockpit
651:Wib 10
636:Wib 74
631:Wib 73
626:Wib 72
621:Wib 71
519:
490:
455:Flight
365:3.0 hr
357:Range:
225:struts
217:rudder
201:Rateau
162:struts
159:faired
53:France
646:Wib 9
616:Wib 7
611:Wib 3
606:Wib 2
601:Wib 1
400:Guns:
270:Crew:
151:chord
33:Role
548:2014
517:ISSN
488:ISBN
320:1 ×
199:. A
86:The
326:V-8
272:One
185:V-8
90:or
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538:.
464:^
452:.
427:^
328:,
179:)
177:hp
173:kW
106:.
578:e
571:t
564:v
550:.
523:.
496:.
384::
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