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词条 Wibault 8 Simoun
释义

  1. Design

  2. Specifications

  3. References

name=Wibault 8 Simounimage=Wibault 8C2 NACA Aircraft Circular No.9.jpgcaption=8C2

}}{{Infobox Aircraft Type

type=Two seat fighter aircraftnational origin=Francemanufacturer=Avions Michel Wibaultdesigner=first flight=May 1926introduced=retired=status=primary user=more users= produced= number built=1[1]program cost= unit cost= developed from=variants with their own articles=
}}

The Wibault 8 or Wib 8 Simoun (Simoon) was a tandem seat, parasol wing fighter aircraft designed and built in France to a 1925 specification which was later withdrawn; only one Wib 8 was completed.

Design

The Wib 8 Simoun was designed around a 1925 specification from the Service Technique de l'Aéronautique (S.T.Aé, Technical Department of Aeronautics) for a two-seat fighter. Wibault's submission was one of a series of parasol wing aircraft, beginning with the Wibault Wib 3 and including the successful Wib 7. Along with the later Wib 12 and the single seat Wib 170, which also used the water-cooled upright V-12 {{convert|500|hp|kW|abbr=on|0}} Hispano-Suiza 12Hb engine, it was the most powerful of the group.

The design and construction of the Wib 8 was similar to that of the earlier aircraft. It was an all- metal machine, the structure mostly Duralumin and the covering narrow aluminium strips applied longitudinally. The parasol wing, built around box spars, was straight edged and of constant chord, braced to the lower fuselage with a pair of parallel struts on each side which met the wing at about mid-span. There were cabane struts over the fuselage and a trailing edge cut-out in the wing over the pilot's cockpit to enhance his visibility. A pair of synchronised {{Convert|7.7|mm|in|3|abbr=on}} Vickers machine guns fixed to the fuselage fired forwards through the propeller arc; in addition the rear cockpit was fitted with a pair of Lewis guns of the same calibre on a Scarff ring. The gunner also had auxiliary flight controls. A braced tailplane was mounted towards the top of the fuselage, together with an angular fin and rudder.

The Wib 8's engine was totally enclosed and drove a two blade propeller. The Mercedes was cooled by a retractable, half-cylindrical radiator on the fuselage underside at the back of the engine. Behind the engine the fuselage was flat sided, like that of the Wib 7. The fighter had a fixed conventional undercarriage with mainwheels on a split axle attached to the fuselage underside, supported by a pair of V-struts; there was a small tailskid.

It was flown for the first time in May 1926 but like other contenders for the contract it failed to meet the S.T.Aé's expectations. The two seat specification was then withdrawn and development of the sole Wib 8 ended.

Specifications

{{Aircraft specs
|ref=Green & Swanborough p.596
|prime units?=met
|genhide=
|crew=Two
|capacity=
|length m=8.95
|length note=
|span m=12.63
|span note=
|height m=3.20
|height note=
|wing area sqm=29.60
|wing area note=
|airfoil=
|empty weight kg=1233
|empty weight note=
|gross weight kg=2064
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=
|eng1 number=1
|eng1 name=Hispano-Suiza 12Hb
|eng1 type=water-cooled upright V-12
|eng1 hp=500
|eng1 note=
|power original=
|more power=
|prop blade number=2
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|perfhide=
|max speed kmh=236
|max speed note=at 2,000 m (6,650 ft)
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=600
|range note=[1]
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=7000
|ceiling note=[1]
|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=18.8 min to 5,000 m (16,405 ft)
|wing loading kg/m2
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|more performance=
|armament=
  • Forward firing guns: 2×{{Convert|7.7|mm|in|3|abbr=on}} synchronised Vickers machine guns in fuselage, 2×{{Convert|7.7|mm|in|3|abbr=on}} Darne machine guns in wings.
  • Rear cockpit: 2×{{Convert|7.7|mm|in|3|abbr=on}} Lewis guns on Scarff ring.

}}{{aircontent
|see also=
|related=
|similar aircraft=
|lists=
}}

References

{{commons category|Wibault 8}}
1. ^{{cite web |url=http://www.aviafrance.com/wibault-8-simoun--aviation-france-1307.htm|title=Wibault 8 Simoum |author= |date= |work= |publisher= |accessdate=28 April 2013}}
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}}{{Wibault aircraft}}

4 : Parasol-wing aircraft|French fighter aircraft 1920–1929|Wibault aircraft|Single-engined tractor aircraft

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