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词条 Nieuport-Delage NiD 37
释义

  1. Design and development

     Related developments 

  2. Specifications for Nieuport-Delage 37 C.1 fighter

  3. References

     Citations  Bibliography 
name=NiD 37 image=Nieuport-Delage 37.tif caption=Nieuport-Deage NiD.37 fighter at the 1922 Paris Show

}}{{Infobox Aircraft Type

type=Single-seat fighter national origin=France manufacturer=Nieuport-Delage designer=E. Dieudonné first flight=April 1923 introduced= retired= status= primary user= more users= produced= number built=1 program cost= unit cost= developed from= variants with their own articles=
}}

The Nieuport-Delage NiD 37 was a single-engine, single-seat monoplane fighter aircraft and racer designed and built in France in the early 1920s. It had a small foreplane to bring the centre of pressure forward. Heavy, slower than expected and with turbo-supercharger problems, development ended without any entering service.

Design and development

Though the NiD 37 has sometimes been termed a sesquiplane,[1] it could be described as a shoulder-wing monoplane with a small foreplane. Its immediate predecessor was the NiD 31, which had a similar flying surface. The two designs had little else in common however.[2]

The fuselage of the NiD 37 was constructed in Nieuport-Delage's standard manner with a monocoque shell of spirally wound and glued tulipwood with a final outer fabric covering. This gave a smooth finish to the circular cross section structure which tapered gently to the tail from a dome-shaped nose housing the {{convert|300|hp|kW|abbr=on|0|disp=flip}} Hispano-Suiza 8Fb water-cooled V-8 engine and its Rateau turbo-supercharger. The engine was mounted with its output shaft low in the nose and drove a two-blade propeller. Though this was of the wooden, fixed-pitch type, it was intended that it would be replaced by a variable-pitch Lavasseur airscrew later. A single, cylindrical Lamblin radiator was suspended below the engine between the undercarriage legs.[1][2]

Dieudonné, the designer of the NiD 37, paid particular attention to the pilot's field of view, and the open cockpit, with screen and faired headrest, was placed well forward, above the engine. To improve the pilot's view downward, the leading edges of the main wing, which were otherwise straight and unswept, were curved in towards the root, meeting the fuselage behind the pilot who could see vertically down between the wing and the trailing edge of the foreplane, aligned with the leading edge of the outer sections of the mainplane and mounted well below on the undercarriage struts. Apart from long, curved tips, this foreplane had straight edges and constant chord; it had a span of about 40% that of the mainplane and less than 20% of its area. Its function was largely to bring the centre of pressure forward. The main wing was slightly tapered away from its roots and with square tips. It was built around four spars and covered in stressed 3-ply, with long-span ailerons. On each side a V-form pair of tubular struts within aerofoil fairings braced the lower fuselage to the wing.[1][2]

The trailing edge of the mainplane had a long fillet reaching almost to the curved leading edge of the broad tailplane; mounted at mid-fuselage, this had strong inboard sweep, decreasing outwards. It carried horn-balanced elevators. The fin was smaller, with a rounded, balanced rudder. The NiD 37 had a fixed, conventional undercarriage with its mainwheels, streamlined with partial (45°) aluminium fairings, mounted on faired V-struts. These had short forward projections to carry the foreplane at axle height.[1][2]

The NiD 37 first appeared in public at the Paris Air Show in December 1922, though it had not then flown. It carried twin {{convert|7.7|mm|in|3|abbr=on}} Vickers machine guns mounted in the nose in front of the cockpit and over the engine. Its first flight took place the following April. Tests proved disappointing as the NiD 37 was heavy compared with its competitors and slower than expected and never achieved the predicted {{convert|250|km/h|mph|abbr=on|0}} top speed. There were also problems with the turbo-supercharger because of the limitations of the high-temperature alloys of the time. As a result of these problems, development was abandoned.[2]

Related developments

A second aircraft was built as a racer with a substantially reduced wing area and a cantilevered upper wing. Some sources list this as a NiD 37, others as the 41. After a carburetor fire during the 1922 Coupe Deutsch, it withdrew and was retired permanently.[3]

Nieuport-Delage also had plans for a larger three seat development of the same concept under the designation NiD.39, also with the pilot over the engine, however with the lack of success of the fighter/racer, it was not proceeded with and the number was reused for an unrelated biplane airliner.

Specifications for Nieuport-Delage 37 C.1 fighter

{{Aircraft specs
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|prime units?=met


|genhide=
|crew=One
|length m=7.16
|length note=
|span m=11.80
|lower span m=
|lower span ft=
|lower span in=
|height m=2.97
|wing area sqm=26.80
|wing area note=total; upper wing {{convert|21.78|m2|sqft|abbr=on}}
|aspect ratio=
|airfoil=
|empty weight kg=980
|gross weight kg=1420
|max takeoff weight kg=
|max takeoff weight lb=
|fuel capacity={{convert|240|L|abbr=on}}


|eng1 number=1
|eng1 name=Hispano-Suiza 8Fb
|eng1 type=upright water cooled V-8
|eng1 hp=300
|eng1 note=
|power original=
|more power=
|prop blade number=2
|prop name=fixed pitch
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=250
|max speed note=at {{cvt|7000|m}} estimated, but not achieved
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise 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=
|wing loading kg/m2
|wing loading lb/sqft=10.8
|wing loading note=including both flying surfaces[1]
|power/mass=0.16 kW/kg (0.095 hp/lb)[1]
|more performance=


|armament=

  • 2 × {{convert|7.7|mm|in|3|abbr=on}} Vickers machine guns fixed in nose

}}{{aircontent
|see also=
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}}

References

{{commons category|Nieuport-Delage NiD 37}}

Citations

1. ^Flight, 1923, p.48
2. ^Green, 1994 , p.438
3. ^Rosenthal, 1997, p.147

Bibliography

{{Refbegin}}
  • {{cite book |last=Green|first=William|first2=Gordon|last2=Swanborough|title=The Complete Book of Fighters |year=1994|publisher=Salamander Books|location=Godalming, UK|isbn=1-85833-777-1|page=438}}
  • {{cite magazine|date=25 January 1923 |title=The Paris Aero Show 1922|magazine=Flight|volume=XV|issue=4|page=48|url=http://www.flightglobal.com/pdfarchive/view/1923/1923%20-%200048.html}}
  • {{cite book|last=Rosenthal |first=Léonard |last2=Marchand |first2=Alain |last3=Borget |first3=Michel |last4=Bénichou |first4=Michel |title=Nieuport 1909-1950 Collection Docavia Volume 38|publisher=Editions Lariviere |location=Clichy Cedex, France |year=1997 |isbn=978-2848900711}}
{{Refend}}{{Nieuport aircraft}}

5 : French fighter aircraft 1920–1929|Nieuport aircraft|Shoulder-wing aircraft|Single-engined tractor aircraft|Sesquiplanes

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