- Flanders F.2
__NOTOC__ Infobox Aircraft
name=Flanders F.2
caption=
type=Single-seat monoplane
manufacturer=Howard Flanders
designer=Howard Flanders
first flight=1911
introduced=
retired=1912
status=Destroyed
primary user=
more users=
produced=
number built=One
variants with their own articles=The Flanders F.2 was a 1910s British experimental single-seat
monoplane aircraft designed and built byHoward Flanders and later converted to a two-seater as the Flanders F.3.Development
Howard Flanders had been an assistant to A.V.Roe when he decided to design his own aircraft. In 1910 he could not get an appropriate engine for it. He started again on another monoplane design, the Flanders F.2 powered by a 60 hp (45 kW) Green engine. The F.2 was a single-seat shoulder-wing monoplane. The wing as usual for the period was braced by wires and kingposts. It had a fixed tailskid landing gear with bicycle-type wheels and a central skid projecting forward from between the wheels. The central skid was to stop the aircraft nosing over on rough ground. It flew for the first time on
8 August 1911 .Later in
1911 the aircraft was modified to include another cockpit forward of the pilot for a passenger. The wingspan was increased and the modified aircraft was re-designated the Flanders F.3. It flew successfully for a number of months until is was destroyed in a fatal accident on13 May 1912 . In 1912 the War Office ordered four monoplanes based on the F.3 and designated theFlanders F.4 Variants
;F.1:Unbuilt experimental monoplane;F.2:Single-seat monoplane powered by a 60hp (45 kW) Green engine.;F.3:F.2 modified as a two-seater with increased wingspan to 42 ft 0 in (12.80m).
pecifications (F.2)
aerospecs
ref=The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishingmet or eng?= eng
crew=One
capacity=
length m=9.68
length ft=31
length in=9
span m=10.67
span ft=35
span in=0
swept m=
swept ft=
swept in=
rot number=
rot dia m=
rot dia ft=
rot dia in=
dia m=
dia ft=
dia in=
width m=
width ft=
width in=
height m=
height ft=
height in=
wing area sqm=18.58
wing area sqft=200
swept area sqm=
swept area sqft=
rot area sqm=
rot area sqft=
volume m3=
volume ft3=
aspect ratio=
empty weight kg=
empty weight lb=
gross weight kg=567
gross weight lb=1250
lift kg=
lift lb=eng1 number=One
eng1 type=Green inline engine
eng1 kw= 45
eng1 hp= 60
eng1 kn=
eng1 lbf=
eng1 kn-ab=
eng1 lbf-ab=
eng2 number=
eng2 type=
eng2 kw=
eng2 hp=
eng2 kn=
eng2 lbf=
eng2 kn-ab=
eng2 lbf-ab=max speed kmh=97
max speed mph=60
max speed mach=
cruise speed kmh=
cruise speed mph=
range km=
range miles=
endurance h=
endurance min=
ceiling m=
ceiling ft=
glide ratio=
climb rate ms=
climb rate ftmin=
sink rate ms=
sink rate ftmin=armament1=
armament2=
armament3=
armament4=
armament5=
armament6=References
* The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing
ee also
aircontent
related=
similar aircraft=
sequence= F.1 • F.2 • F.3 • F.4 • B.2
lists=see also=
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