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词条 Wendt W-2 Swift
释义

  1. Design and development

  2. Specifications

  3. Notes

  4. References

name=W-2 Swift image= caption=

}}{{Infobox Aircraft Type

type=Two-seat cabin monoplane national origin=United States manufacturer=Wendt Aircraft Corporation designer= first flight=1939 introduced= retired= status= primary user= more users= produced= number built=1 program cost= unit cost= developed from= variants with their own articles=
}}

The Wendt W-2 Swift was a two-seat, single-engine, braced high-wing monoplane built in the United States just before World War II. Only one was built.

Design and development

The Wendt Aircraft Co. was formed in February 1939 to build the W-2 Swift, the prototype of which turned out to be their only product. It had a high braced wing, built around two spruce spars. The ribs were made of spruce and birch with steel wire internal bracing. Its leading and trailing edges were metal, with fabric elsewhere. The wing was braced on either side by pairs of V-form, steel struts mounted on the lower fuselage longerons. The fuselage was a chrome molybdenum steel tube structure, fabric covered over plywood formers and spruce stringers. The enclosed cabin, which seated two side-by-side with dual control, was under the wing, with the 90 hp (67 kW) single row radial LeBlond engine mounted immediately ahead of it under a clean NACA cowling in the short nose.[1]

The tail unit was metal framed and fabric covered. The tailplane was externally braced and the elevators carried trim tabs. The fin was straight edged but the rudder, which extended to the bottom of the fuselage and worked in a cut-out between the elevators, had a full, curved trailing edge.[1]

The Swift had a fixed, conventional undercarriage with faired main legs and wheels, rubber shock absorbers and half-axles hinged under the fuselage. The main wheels had brakes and the tailwheel was steerable.[1]

Specifications

{{Aircraft specs
|ref=Jane's All the World's Aircraft 1941[1]
|prime units?=imp


|genhide=
|capacity=Two
|length ft=20
|length in=0
|length note=
|span ft=30
|span in=0
|span note=
|height ft=6
|height in=8.5
|height note=
|wing area sqft=145
|wing area note=
|aspect ratio=
|airfoil=
|empty weight lb=778
|empty weight note=
|gross weight lb=1400
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=LeBlond (Ken Boyce) 5F[5]
|eng1 type=5-cylinder radial
|eng1 hp=90
|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 mph=130
|max speed note=
|cruise speed mph=120
|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 miles=525
|range note=at cruising speed
|endurance=
|ceiling m=
|ceiling ft=16000
|ceiling note=service ceiling
|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|wing loading lb/sqft=10.0
|wing loading note=
|power/mass=0.067 hp/lb (0.11 kW/kg)
|more performance=

  • Landing speed: 35 mph (56 km/h)

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

Notes

1. ^{{cite book |title= Jane's All the World's Aircraft 1941|last= Bridgman |first= Leonard |coauthors= |edition= |year=1941|publisher=Sampson, Low, Marston and Co. Ltd|location= London|page=233c}}
2. ^{{cite web |url=http://www.aerofiles.com/_wa.html|title=Wendt |author= |date= |work= |publisher= |accessdate=3 August 2012}}

References

{{reflist|refs=[1][2]
}}

3 : United States civil utility aircraft 1930–1939|High-wing aircraft|Aircraft first flown in 1939

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