请输入您要查询的百科知识:

 

词条 Darmstadt D-18
释义

  1. Design and development

  2. Operational history

  3. Specifications

     Description 

  4. References

  5. External links

name= Darmstadt D-18image=Bundesarchiv Bild 102-10158, Piloten des internationalen Europa-Rundflugs.jpgcaption=Rudolf Neininger (left) with his crewman in front of the D-18 during Challenge 1930

}}{{Infobox Aircraft Type

type=Sportsplanemanufacturer= Akaflieg Darmstadtdesigner=first flight= 1929introduced=retired=status=Prototypeprimary user=Germanymore users=produced=1929number built=1unit cost=variants with their own articles=Darmstadt D-22
}}

The Darmstadt D-18 was a German light sports aircraft that was designed and built in the late-1920s by the Akaflieg Darmstadt of the Darmstadt University of Technology.

Design and development

The aircraft was designed by F. Fecher and students in the aeronautical engineering department of Darmstadt University. It was a development of the D-16 project, that was designed for a sports aircraft contest organized by Idaflieg in 1926. The D-16 design with a 40-horsepower (hp) engine won the first prize, but was not built as the designer decided to strengthen the construction and fit a more powerful 88 hp Armstrong Siddeley Genet radial engine. The result was the D-18, a single aircraft was built in 1929.

The aircraft featured a quite unorthodox layout, being a cantilever biplane, with an upper wing placed low above a fuselage and ahead of a lower wing. Particular thought was given to aerodynamics and lightness and the aircraft was small, with a streamlined profile. Initially the D-18 had two open cockpits, but by 1930 it had been modified and fitted with a closed canopy covering both cockpits.

Operational history

The aircraft carried the registration of D-1561. It took part in the Challenge 1929 international tourist plane contest, piloted by Johannes Nehring, being one of the fastest planes in the contest. It was the best aircraft in the fuel consumption trial and, along with two other aircraft, won the first part of the contest - the technical trials. However, the D-18 dropped out due to a forced landing near Września before Poznań on 11 August 1929, during a rally around Europe, because of a fuel pipe clogging. The aircraft turned over and suffered damage; its passenger was injured.

The aircraft was repaired and, now fitted with an enclosed cabin, it took part in another contest, Challenge 1930, again piloted by Rudolf Neininger. On 26 July 1930, during a rally around Europe the D-18 was forced to ditch in the Mediterranean Sea between Barcelona and Nîmes due to breaking a piston. The crew was rescued by a passing ship that also recovered the wreckage.

Specifications

Description

Wooden construction cantilever biplane of extreme stagger. Fuselage oval in cross-section, plywood covered. Single-spar wings, plywood and canvas covered. Aileron on lower wing only Wings were dismounted and folded. Two crew cockpits in tandem, later covered with a common multi-part canopy. Fixed landing gear with a rear skid. Five-cylinder radial engine in the cowled nose with its cylinders projecting for cooling. Two-blade propeller.

{{Aircraft specs
|ref=Les Ailes, March 1929
|prime units?=met


|genhide=
|crew=Two
|length m=6.14
|length note=
|span m=7.20
|span note=
|upper span m=
|upper span ft=
|upper span in=
|upper span note=
|lower span m=
|lower span ft=
|lower span in=
|lower span note=
|height m=2.62
|height note=
|wing area sqm=12.10
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=400
|empty weight note=approximately
|gross weight kg=
|gross weight lb=
|gross weight note=650
|max takeoff weight kg=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Armstrong-Siddeley Genet
|eng1 type=5-cylinder radial
|eng1 hp=80
|eng1 note=
|more power=
|prop blade number=2
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=200
|max speed note=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|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=800
|range note=
|endurance=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=3 min to {{convert|1000|m|ft|abbr=on}}
|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=
|thrust/weight=
|more performance=
}}

References


}}
  • Marian Krzyżan: "Międzynarodowe turnieje lotnicze 1929-1934", Warsaw 1988, {{ISBN|83-206-0637-3}} (Polish language)

External links

{{Commons category|Darmstadt D-18}}
  • D-18 3-view Akaflieg Darmstadt page
  • [https://www.akaflieg.tu-darmstadt.de/prototypen/ D-18 photo Akaflieg Darmstadt page]
  • [https://web.archive.org/web/20070612165439/http://www.generalaviationnews.com/editorial/articledetail.lasso?-token.key=10217&-token.src=column&-nothing Peter M. Bowers, Darmstadt biplanes- article at General Aviation News]
{{Akaflieg Darmstadt aircraft}}

5 : German sport aircraft 1920–1929|Akaflieg Darmstadt aircraft|Single-engined tractor aircraft|Biplanes|Aircraft first flown in 1929

随便看

 

开放百科全书收录14589846条英语、德语、日语等多语种百科知识,基本涵盖了大多数领域的百科知识,是一部内容自由、开放的电子版国际百科全书。

 

Copyright © 2023 OENC.NET All Rights Reserved
京ICP备2021023879号 更新时间:2024/9/27 10:20:02