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词条 Fauvel AV.29
释义

  1. Design

  2. Variants

  3. Specifications (AV.29M)

  4. References

name=Fauvel AV.29 image= caption=

}}{{Infobox Aircraft Type

type=Flying wing transport national origin=France manufacturer= designer=Charles Fauvel first flight=none number built=0 developed from= variants with their own articles=
}}

The Fauvel AV.29 was a design for a transport plane by Charles Fauvel in the late 1930s.

Design

The AV.29, a small two-engine tourism/transport aircraft, to be powered by two Régnier 4F.0 engines was also intended to be a flying scale model for the two-seat AV.29 C2 fighter (M for Maquette - model). The much larger AV.29 C2 two-seat fighter was planned to use either, 14-cylinder Gnome-Rhône 14M Mars radial engines or 12-cylinder Hispano-Suiza 12Y engines. However, the AV.29, in both forms, remained a paper project only.[1]

Variants

Data from:Charles Fauvel and his Flying Wings[1]
AV.29M
Projected 4-seat tail-less touring aircraft powered by two Régnier 4F.0 engines
AV.29 C2
Much enlarged {{cvt|12.48|m}} span two-seat fighter, to have been powered by a 14-cylinder Gnome & Rhône Mars radial engines or 12-cylinder Hispano-Suiza 12Y engine.

Specifications (AV.29M)

{{Aircraft specs
|ref=Charles Fauvel and his Flying Wings[1]
|prime units?=met


|genhide=
|crew=1
|capacity 3 pax
|length m=4.44
|length note=including elevator
|span m=10.96
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=19.96
|wing area note=
|swept area note=
|aspect ratio=
|airfoil=
|empty weight kg=786
|empty weight note=
|gross weight kg=1143
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=2
|eng1 name=Régnier 4F.0
|eng1 type=12-cylinder radial piston engines
|eng1 hp=140
|eng1 note=
|more power=
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=330
|max speed note=
|cruise speed kmh=295
|cruise speed note=

  • Minimum speed: {{cvt|92|km/h|mph kn}}

|stall speed kmh=
|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=
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=9300
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=8.8
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|more performance=
}}

References

1. ^{{cite web |title=Charles Fauvel and his Flying Wings |url=http://www.nurflugel.com/Nurflugel/Fauvel/e_AV29.htm |website=www.nurflugel.com |accessdate=1 March 2019 |language=French}}
{{Fauvel aircraft}}

4 : Tailless aircraft|Flying wings|French aircraft 1930–1939|Fauvel aircraft

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