Nieuport II
{{short description|French pre-WW1 racing aircraft}}
{{about|the pre-ww1 Nieuport II racer|the World War 1 Nieuport 11 fighter|Nieuport 11}}
{{Infobox aircraft begin
|name=Nieuport II |image=Nieuport 2N musee du Bourget P1010306.JPG |caption=Surviving late production Nieuport II.N at the Musée de l'Air et de l'Espace }}{{Infobox aircraft type |type=Sport aircraft/Racer |national origin=France |manufacturer=Nieuport |first flight=1910 |produced=1910-1914 }} |
The Nieuport II was a mid-wing monoplane racing or sport aircraft built by the Société Anonyme des Établissements Nieuport between 1910 and 1914 and was noted for its high performance using a small twin-cylinder engine, and winning many races, primarily in France before being used as a trainer during World War I by French flying schools.
Background
Édouard Nieuport was the owner of a small company which produced spark plugs and magnetos for the automobile industry, and he became involved with aviation through working on the electrical equipment of Henri Farman's Voisin biplane. In 1908 he started constructing his first aircraft, a small monoplane powered by a 20 hp (15 kW) Darracq engine and succeeded in making some brief straight-line flights in it during 1909, but the aircraft, along with many others, was destroyed in the floods which struck Paris in January 1910.Opdycke 1999 p.189
Development and design
File:Nieuport Monoplane Catalogue.jpg
The Nieuport II was the subject of extensive research carried out by the Nieuport brothers in conjunction with the Eiffel Laboratories and benefited from input from Robert Esnault-Pelterie, who had designed his own low-drag monoplane. The result was a wire-braced monoplane with only a single pair of bracing wires on each side, supplemented with a single pair of control wires to warp the wings for lateral control. The airfoil section was unusual in having a fairly thick (for the period), but sharp leading edge, with the undersides rising up to thin the airfoil out over the majority of the chord. The upper wires led to a pyramidal cabane and the pilot was nearly fully enclosed in the fuselage, with only his head exposed. Initially the undercarriage consisted of a single central skid attached to the fuselage by two inverted V struts, bearing a transverse leaf spring with a wheel on each end. When first flown the tail surfaces consisted of a semicircular horizontal stabiliser mounted on top of the rear of the fuselage, behind which was a universally-jointed assembly combining a rectangular elevator with a pair of rudders. The controls used the joystick to provide yaw (rudder) and pitch (elevator) control, while foot pedals operated the wing warping for lateral control, the pedals moving a torque tube which ran diagonally backwards to the rear V-strut of the undercarriage, where the warping wires were attached.
Late examples were available with the modern arrangement as a factory option, using the pedals to control the rudder, as was used on the contemporary Blériot and Deperdussin aircraft. A variety of engines were used, starting with the Darracq, which, despite being developed specifically for Nieuport, proved unsatisfactory, and a variety of engines were tried before the Nieuport brothers developed their own twin-cylinder, horizontally-opposed engine.
Operational history
File:Nieuport II.G Helen Michelin cup.jpg]]
On 11 May Nieuport succeeded in breaking the world speed record for all distances up to 100 km flying a Nieuport II powered by a {{convert|28|hp|abbr=on}} Nieuport engine. His highest recorded speed was {{convert|119.63|km/h|abbr=on}}[http://www.flightglobal.com/pdfarchive/view/1911/1911%20-%200445.html "New Speed Records"]Flight 20 May 1911
Three were flown in the 1911 Gordon Bennett Trophy at Eastchurch: one, flown by Charles Weymann and powered by a {{convert|100|hp|abbr=on}} Gnome double Omega, won the competition with a speed of 126.67 km/h (78.71 mph); a second, powered by a {{convert|70|hp|abbr=on}}
Gnome Lambda and flown by Edouard Nieuport, placed third: the third, flown by M Chevalier and powered by a {{convert|28|hp|abbr=on}} Nieuport engine, failed to finish.[http://www.flightglobal.com/pdfarchive/view/1911/1911%20-%200587.html "Table of Cumulative Lap Times"]Flight 8 July 1911.
Variants
;II.D:18 hp twin-cylinder horizontally opposed Darraq 25hp O-2 engine
;II.A:40 hp fan type Anzani engine
;II.G:Gnome rotary engines, of 50, 70 or 100 hp
;II.N:28 hp twin-cylinder horizontally opposed Nieuport engine.
;II.H:Floatplane variant (offered but not built)
Operators
Most examples were used by individuals, however a small number were purchased by military air arms including:
;{{ARG}}
;{{FRA}}
- Aéronautique Militaire
- Used for flight training, including as a flightless ground trainer commonly known as a Penguin.
;{{flagicon|Thailand|1855}} Siam
- Royal Siamese Air Service
- First aircraft of Royal Siamese Air Force
Survivors and replicas
- late-production Nieuport II.N at the Musée de l'Air et de l'Espace, Le Bourget near Paris
- A taxi-able replica is at Old Rhinebeck Aerodrome in Poughkeepsie, New York state
Specifications (28 hp Nieuport engine)
{{Aircraft specs
|ref={{cite web|url=http://www.aviafrance.com/nieuport-ii-n-aviation-france-10034.htm|title=Nieuport II N|accessdate= 21 May 2012}}
|prime units?=met
|genhide=
|crew=one
|length m=7.15
|lengthe ft=
|length ft= |
|length in=
|length note=
|span m= 8.65
|span ft=
|span in=
|span note=
|height m= 2.60
|height ft=
|height in=
|height note=
|wing area sqm= 14
|wing area sqft=
|wing area note=
|airfoil=
|empty weight kg=240
|empty weight lb= |
|empty weight note=
|gross weight kg=340
|gross weight lb= |
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=
|eng1 number=1 |
|eng1 name=Nieuport |
|eng1 type=2-cylinder Horizontally opposed air-cooled
|eng1 kw=
|eng1 hp=28
|eng1 shp=
|eng1 note=
|prop blade number=2 ||prop name= ||prop dia m= ||prop dia ft= ||prop dia in= ||prop dia note=
|rot number= ||rot dia m= ||rot dia ft= ||rot dia in= ||rot area sqm= ||rot area sqft= ||rot area note=
|perfhide=
|max speed kmh=115
|max speed mph= |
|max speed kts=
|max speed note= ||max speed mach=
|cruise speed kmh= ||cruise speed mph= ||cruise speed kts= ||cruise speed note=
|stall speed kmh= ||stall speed mph= ||stall speed kts= ||stall speed note=
|range km= ||range miles= ||range nmi= ||range note=
|endurance=
|ceiling m= ||ceiling ft= ||ceiling note=
|climb rate ms= ||climb rate ftmin= ||climb rate note= ||time to altitude=
|lift to drag=
|wing loading kg/m2= ||wing loading lb/sqft= ||wing loading note=
|fuel consumption kg/km= ||fuel consumption lb/mi=
|power/mass= ||thrust/weight=
}}
See also
{{aircontent
|related=
|similar aircraft=
|lists=
|see also=
}}
References
{{commons category|Nieuport II}}
=Citations=
{{Reflist|1}}
=Bibliography=
{{refbegin}}
- Davilla, Dr. James J. and Arthur Soltan. French Aircraft of the First World War, Flying Machines Press, Mountain View California, 1997, {{ISBN|0-9637110-4-0}}
- Kowalski, Tomasz J. Nieuport 1-27, Kagero, Lublin, 2003, {{ISBN|83-89088-09-6}}
- Opdycke, Leonard E. French Aeroplanes Before The Great War. Atglen, PA: Achiffer, 1999. {{ISBN|0-7643-0752-5}}
- Pommier, Gerard. Nieuport 1875-1911 - A Biography of Edouard Nieuport, Schiffer Publishing, Atglen, PA, 2002 {{ISBN|0-7643-1624-9}}
- Rimmell, Ray. World War I Survivors, Aston Publications, Bucks, 1990, {{ISBN|0-946627-44-4}}
{{refend}}
{{Nieuport aircraft}}
Category:1910s French sport aircraft
Category:1910s French military trainer aircraft
Category:Single-engined tractor aircraft