Blériot VII: Difference between revisions
m Robot - Moving category French experimental aircraft 1900-1909 to Category:French experimental aircraft 1900–1909 per CFD at Wikipedia:Categories for discussion/Log/2011 September 20. |
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==Specifications== |
==Specifications== |
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{{Aircraft specs |
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{{aerospecs |
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|ref=Opdycke 1990, p.49 |
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|met or eng?=<!-- eng for US/UK aircraft, met for all others -->met |
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|prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show --> |
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General characteristics |
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|crew= |
|crew=1 |
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|capacity= |
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|length m= |
|length m=9 |
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|length ft= |
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|length in= |
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|span |
|span m=11 |
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|span |
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|dia m=<!-- helicopters --> |
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|dia ft=<!-- helicopters --> |
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|dia in=<!-- helicopters --> |
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|height m= |
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|wing area sqm=25.0 |
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|wing area |
|wing area sqm=25 |
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|aspect ratio=<!-- sailplanes --> |
|aspect ratio=<!-- give where relevant eg sailplanes --> |
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|empty weight kg= |
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|empty weight lb= |
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|empty weight note= |
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|gross weight kg=425 |
|gross weight kg=425 |
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|gross weight lb= |
|gross weight lb= |
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|gross weight note= |
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|max takeoff weight kg= |
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|max takeoff weight lb= |
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|fuel capacity= |
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|eng1 type=[[V8 engine|V-8]] water-cooled [[piston engine]] |
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|eng1 hp=50<!-- prop engines --> |
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|eng1 kn=<!-- jet/rocket engines --> |
|eng1 kn=<!-- jet/rocket engines --> |
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|eng1 lbf=<!-- jet/rocket engines --> |
|eng1 lbf=<!-- jet/rocket engines --> |
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|eng1 lbf-ab=<!-- afterburners --> |
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|eng2 kw=<!-- prop engines --> |
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|eng2 hp=<!-- prop engines --> |
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|eng2 kn-ab=<!-- afterburners --> |
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|eng2 lbf-ab=<!-- afterburners --> |
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|prop blade number=2<!-- propeller aircraft --> |
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|prop dia ft=9<!-- propeller aircraft --> |
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Performance |
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|max speed mach=<!-- supersonic aircraft --> |
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|endurance min=<!-- if range unknown --> |
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|glide ratio=<!-- sailplanes --> |
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|climb rate ms= |
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|climb rate ftmin= |
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|time to altitude= |
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|sink rate ftmin=<!-- sailplanes --> |
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|sink rate note= |
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|lift to drag= |
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|wing loading kg/m2 |
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|wing loading lb/sqft= |
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|wing loading note= |
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|power/mass= |
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|thrust/weight= |
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|more performance= |
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|armament1= |
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|armament2= |
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|armament3= |
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}} |
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==References== |
==References== |
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{{reflist}} |
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===Bibliography=== |
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* {{cite book |last= Elliott |first= Bryan A. |title=Blériot: Herald of an Age |year=2000 |publisher=Tempus|location=Stroud |isbn=0-7524-1739-8 }} |
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* {{cite book |last= Opdycke |first= Leonard E. |title=French Aircraft Before the Great War |year=1990 |publisher=Schiffer |location=Atglen, PA |isbn=0-7643-0752-5 }} |
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* {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=161 }} |
* {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=161 }} |
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* Devaux, Jean and Michel Marani. "Les Douze Premiers Aéroplanes de Louis Blériot". ''Pegase'' No 54, May 1989. |
* Devaux, Jean and Michel Marani. "Les Douze Premiers Aéroplanes de Louis Blériot". ''Pegase'' No 54, May 1989. |
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==External links== |
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* [http://www.pbs.org/wgbh/nova/bleriot/imag-nf.html Nova: A Daring Flight] |
* [http://www.pbs.org/wgbh/nova/bleriot/imag-nf.html Nova: A Daring Flight] |
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* [http://www.earlyaviators.com/ebleriot1.htm earlyaviators.com] |
* [http://www.earlyaviators.com/ebleriot1.htm earlyaviators.com] |
Revision as of 09:18, 5 March 2012
VII | |
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![]() | |
Role | Experimental aircraft |
Manufacturer | Louis Blériot |
Produced | 1907 |
Number built | 1 |
The Blériot VII was an early French aeroplane built by Louis Blériot. Inspired by his success with the tandem wing configuration of the Blériot VI, he continued this line of development in October 1907. The rear wing of his new design was somewhat smaller than the forward wing and therefore represents another step toward the configuration that would later be adopted as the basis for the vast majority of aircraft. The tail surfaces could be moved together, to act as elevators, or independently to act as ailerons, as one of the first known manifestations of what would become elevons in designs of later decades.
On 5 and 6 November, trials at Issy-les-Moulineaux revealed structural weaknesses which Blériot addressed before making a flight of 500 m at 90 km/h (1,640 ft at 56 mph) on November 16. Many other successful flights were carried out before the aircraft was destroyed on December 18.
Specifications
Data from Opdycke 1990, p.49
General characteristics
- Crew: 1
- Length: 9 m (29 ft 6 in)
- Wingspan: 11 m (36 ft 1 in)
- Wing area: 25 m2 (270 sq ft)
- Gross weight: 425 kg (937 lb)
- Powerplant: 1 × Antoinette V-8 water-cooled piston engine, 37 kW (50 hp)
- Propellers: 2-bladed, 2.7 m (9 ft) diameter
References
Bibliography
- Elliott, Bryan A. (2000). Blériot: Herald of an Age. Stroud: Tempus. ISBN 0-7524-1739-8.
- Opdycke, Leonard E. (1990). French Aircraft Before the Great War. Atglen, PA: Schiffer. ISBN 0-7643-0752-5.
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 161.
- Devaux, Jean and Michel Marani. "Les Douze Premiers Aéroplanes de Louis Blériot". Pegase No 54, May 1989.
External links
See also