| 词条 | Focke-Wulf A 16 | |||||||||||||||
| 释义 |
The Focke-Wulf A.16 was a German three/four passenger light transport monoplane designed by Heinrich Focke and Georg Wulf and was the first design built by the newly formed Focke-Wulf company. DevelopmentWith the success of their earlier designs, Focke and Wulf formed the Focke-Wulf company in 1924 and their first design was an all-wood three/four passenger airliner or light transport, the A.16, first flown by Georg Wulf on 23 June 1924. At least 20 aircraft were built; according to Airbus Industrie, Bremen, 23 were built. Airbus has built another one in the last ten years{{when?|date=November 2015}}, though not airworthy, which is on display at Bremen Airport. The A.16 was a high-wing cantilever monoplane of conventional configuration. The wing used a thick airfoil. The pilot sat in an open cockpit above the wing while the passengers were carried in the enclosed fuselage below. The tailskid undercarriage featured large wheels mounted on each side of the fuselage. Variants
Variant powered by a 100 hp (75 kW) Mercedes D.I engine.[1]
Variant powered by an 85 hp (63 kW) Junkers L1a engine.[2]
Variant powered by a 100 hp (75 kW) Siemens-Halske Sh 12 engine.[2]
Variant powered by a 120 hp (89 kW) Mercedes D.II or D.IIa engine.[2] Specifications (A.16c){{Aerospecs|ref=The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985), 1985, Orbis Publishing, Page 1835 |met or eng?=met |crew=one |capacity=three–four |length m=8.5 |length ft=27 |length in=10{{frac|3|4}} |span m=13.90 |span ft=45 |span in=7{{frac|1|4}} |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=2.30 |height ft=7 |height in=6{{frac|1|2}} |wing area sqm=27.1 |wing area sqft=291[3] |swept area sqm= |swept area sqft= |rot area sqm= |rot area sqft= |volume m3= |volume ft3= |aspect ratio= |empty weight kg=570 |empty weight lb=1256 |gross weight kg=970 |gross weight lb=2138 |lift kg= |lift lb= |eng1 number=1 |eng1 type=Siemens-Halske Sh 11 7-cylinder radial piston engine |eng1 kw=56 |eng1 hp=75 |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=135 |max speed mph=84 |max speed mach= |cruise speed kmh= |cruise speed mph= |range km=550 |range miles=342 |endurance h= |endurance min= |ceiling m=2500 |ceiling ft=8200 |glide ratio= |climb rate ms= |climb rate ftmin= |sink rate ms= |sink rate ftmin= |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }}{{Aircontent |see also= |related= |similar aircraft= |sequence= |lists= }} References1. ^Stroud Aeroplane Monthly January 1987, pp. 41–42. 2. ^1 2 Stroud Aeroplane Monthly January 1987, p. 42. 3. ^Flight 15 January 1925, p. 27.
External links{{commons category|Focke-Wulf A 16}}
5 : German airliners 1920–1929|Focke-Wulf aircraft|Single-engined tractor aircraft|High-wing aircraft|Aircraft first flown in 1924 |
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