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Hurel-Dubois HD.10

From Wikipedia, the free encyclopedia
HD.10
RoleResearch aircraft
Type of aircraft
National originFrance
ManufacturerHurel-Dubois
First flight25 August 1948
Retired28 September 1954
Number built1

TheHurel-Dubois HD.10 was a French research aircraft first flown in 1948 to investigate Maurice Hurel's ideas abouthigh aspect ratio wings. It was a single-seat monoplane with a retractable tricycle undercarriage andtwin tails, featuring a very high aspect-ratio wing of 32.5:1. This was mounted above the aircraft's enclosed cockpit and braced with struts. Construction was of metal throughout. Between 1948 and 1954, this aircraft accumulated some 218 hours and 27 minutes of flight time and is now preserved in theMusée de l'Air et de l'Espace in Paris.

Design and development

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The French aircraft designer Maurice Hurel set up the Société des Avions Hurel-Dubois, with the industrialist Léon-Joseph Dubois, in November 1947, to develop Hurel's theories about the use of high aspect ratio wings.[1] To demonstrate the practicality of these ideas, Hurel designed a single-engined prototype, the HD.10, with construction entrusted to theÉtablissements Pierre Levasseur.[2]

The HD.10 was a high-wingedtractor configurationmonoplane with the metal wing braced by singlelift struts to the fuselage.Fowler flaps were fitted to the wing. The fuselage was of fabric-covered steel tube construction with the pilot sitting in an enclosedcockpit under the trailing edge of the wing. Atwin tail was fitted, and the aircraft had a manually actuated retractabletricycle landing gear. The aircraft was initially powered by a 40 hp (30 kW)Mathis engine.[3][4]

The aircraft made its first flight, with Hurel at the controls, on 25 August 1948.[2] The aircraft was underpowered with the Mathis, and it was re-engined with a 75 hp (56 kW)Praga D. Testing at theCentre d'Essais en Vol resulted in the aircraft's vertical tail surfaces being enlarged.[5] It made its final flight on 20 June 1954, having completed more than 218 flight hours. It was then delivered to theMusée de l'Air atParis–Le Bourget Airport for preservation and display.[5]

Specifications

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Data from aviafrance[6]

General characteristics

  • Crew: 1
  • Length: 5.15 m (16 ft 11 in)
  • Wingspan: 12.00 m (39 ft 4 in)
  • Height: 1.55 m (5 ft 1 in)
  • Wing area: 4.50 m2 (48.4 sq ft)[4]
  • Aspect ratio: 32.5:1[4]
  • Gross weight: 480 kg (1,058 lb)
  • Powerplant: 1 ×Praga D air-cooledflat four, 56 kW (75 hp)

Performance

  • Maximum speed: 250 km/h (160 mph, 130 kn)
  • Range: 1,000 km (620 mi, 540 nmi)
  • Service ceiling: 5,000 m (16,000 ft)

References

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  1. ^Carbonel 2022, p. 85
  2. ^abCarbonel 2022, p. 86
  3. ^Carbonel 2022, pp. 86–87
  4. ^abcBridgman 1951, p. 127c
  5. ^abCarbonel 2022, p. 87
  6. ^Parmentier, Bruno."Hurel-Dubois HD-10".Aviafrance. Retrieved4 January 2014.
  • Bridgman, Leonard (1951).Jane's All the World's Aircraft 1951–52. London: Sampson Low, Marston & Company, Ltd.
  • Carbonel, Jean-Christophe (October 2022). "Database: Hurel-Dubois Aircraft".Aeroplane. Vol. 50, no. 10. pp. 83–99.ISSN 0143-7240.
  • Taylor, Michael J. H. (1989).Jane's Encyclopedia of Aviation. London: Studio Editions. pp. 523–24.
  • World Aircraft Information Files. London: Bright Star Publishing. pp. File 896 Sheet 30.

External links

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Wikimedia Commons has media related toHurel-Dubois HD.10.
Hurel-Dubois [fr] aircraft
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