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词条 Wier RDW-2 Draggin' Fly
释义

  1. Design and development

  2. Specifications

  3. References

  4. External links

name=RDW-2 Draggin' Fly image= caption=

}}{{Infobox Aircraft Type

type=Single seat lightweight homebuilt national origin=United States manufacturer= designer=Ronald Wier first flight=May 1972 introduced= retired= status= primary user= more users= produced= number built=1 program cost= unit cost= developed from= variants with their own articles=
}}

The Wier RDW-2 Draggin' Fly was a homebuilt light aircraft, designed in the United States in the 1970s, aimed at fairly inexperienced builders and flyers. Plans were available but only one was built.

Design and development

The Draggin' Fly was designed to be easy to build, to have good short field characteristics and to have control characteristics matched to the skills of less experienced pilots. A four-cylinder Volkswagen air-cooled engine was selected for reliability and ease of maintenance. The sole example was constructed over ten months without plans, though a rib jig and propeller plot were used. It was first flown in May 1972.

The Draggin' Fly had a constant chord parasol wing, built around two spruce spars and having slight dihedral. The wing was Dacron covered and carried no flaps; the ailerons were aluminium with a full span torque tube. It was held well above the fuselage on a pair of V-shaped bracing struts, assisted by inverted V-cabane struts fore and aft of the cockpit. The fuselage was a steel tube structure and Dacron covered over the forward, pod like part that housed the engine and cockpit but open and triangular in section as it extended rearwards into a tailboom at cabane height. The tail surfaces were again Dacron covered steel, wire braced with the tailplane placed at the bottom of the boom and with the lower rudder and a small ventral fin projecting below it. The Draggin' Fly had a fixed tricycle undercarriage, the mainwheels mounted on two V-form struts and half-axles hinged to the fuselage underside. All undercarriage legs used spring and rubber in compression type shock absorbers; the nose wheel was steerable.

For its first flight and first eight hours of flight testing the Draggin' Fly was powered by a 36 hp (29 kW), 1.2 L Volkswagen engine but this was then replaced by a more powerful Volkswagen variant producing 50 hp (37 kW). Plans for amateur building were produced in March 1974.

Specifications

{{Aircraft specs
|ref=Jane's All the World's Aircraft 1974–75
|prime units?=imp


|genhide=
|crew=One
|capacity=
|length ft=17
|length in=5
|length note=
|span ft=24
|span in=5
|span note=
|height ft=6
|height in=10
|height note=
|wing area sqft=110
|wing area note=
|aspect ratio=
|airfoil=USA 35B
|empty weight lb=470
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight lb=688
|max takeoff weight note=
|fuel capacity= 8.0 US gal (6.7 Imp gal; 30 L)
|more general=


|eng1 number=1
|eng1 name=1.6 L (98 cu in) modified Volkswagen
|eng1 type=air-cooled flat four
|eng1 hp=50
|eng1 note=
|power original=
|more power=
|prop blade number=2
|prop name=hand carved mahogany
|prop dia ft=4
|prop dia in=4
|prop dia note=


|perfhide=
|max speed mph=70
|max speed note=at sea level
|cruise speed mph=65
|cruise speed note=at sea level
|stall speed mph=32
|stall speed note=
|never exceed speed mph=100
|never exceed speed note=
|range miles=170
|range note=no reserves
|endurance=
|ceiling ft=4000
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ftmin=200
|climb rate note=at sea level
|time to altitude=
|lift to drag=
|wing loading lb/sqft=6.25
|wing loading note=maximum
|power/mass=
|thrust/weight=
|more performance=

  • Take-off run: 150 ft (46 m)
  • Landing run: 200 ft (61 m)

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

References


}}

External links

  • USA35B airfoil

4 : Homebuilt aircraft|United States sport aircraft 1970–1979|Parasol-wing aircraft|Aircraft first flown in 1972

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