Jump to content

HW-4 Flamingo

From Wikipedia, the free encyclopedia

This is the current revision of this page, as edited by 176.3.88.11 (talk) at 11:00, 5 August 2024 (added „Rotter Nemere“ as: ‚see also‘ link). The present address (URL) is a permanent link to this version.

(diff) ← Previous revision | Latest revision (diff) | Newer revision → (diff)
HW-4 Flamingo
Role Sailplane
National origin Brazil
Manufacturer Kurt Hendrich
Designer Hans Widmer
First flight 1946
Number built 1

The HW-4 Flamingo, was a Brazilian single-seat sailplane aircraft designed and manufactured for general flying.[1]

Design and development

[edit]

The Flamingo was built in Bauru in 1944, designed by Kurt Henrich and Hand Widmer, it resembled the high-performance German gliders of the time. When designing it, Widmer chose a profile with little penetration, but high elevation index. He made more than 40 drawings, and it was with these that the team started the work. Despite the great performance at low speed, it was not adequate to consider it a racing sailplane. The wings profile were strong cambered. Lighter than contemporary German DFS Weihe, though of similar general dimensions.[2]

Construction

[edit]

It was made largely of domestic wood; the outside was made with plywood and painted linho.[2]

Operational history

[edit]

It was based at the Aeroclube de Bauru while it was operational. He has won numerous Brazilian sailing championships, and several categories. It was retired for a structural reform in 2002 and continued flying until 2006. Its prefix was PT-PAY.[1]

Specifications

[edit]

Data from Pereira de Andrade 1986, p. 101, Simons 2006, p. 26

General characteristics

  • Crew: 1
  • Length: 7.80 m (25 ft 7 in)
  • Wingspan: 18 m (59 ft 1 in)
  • Wing area: 18 m2 (190 sq ft)
  • Aspect ratio: 18
  • Airfoil: Göttingen 539
  • Empty weight: 205 kg (452 lb)
  • Max takeoff weight: 330 kg (728 lb)

Performance

  • Maximum speed: 220 km/h (140 mph, 120 kn)
  • Cruise speed: 104 km/h (64 mph, 56 kn)
  • Maximum glide ratio: 1:28
  • Rate of sink: 0.56 m/s (110 ft/min)
  • Wing loading: 18.4 kg/m2 (3.8 lb/sq ft)

See also

[edit]

Aircraft of comparable role, configuration, and era

References

[edit]
  1. ^ a b Pereira de Andrade, Roberto (1986). A Construção Aeronáutica no Brasil 1910/1976. São Paulo. pp. 119–121. ISBN 9788585262693.{{cite book}}: CS1 maint: location missing publisher (link)
  2. ^ a b Simons, Martin (2006). Sailplanes 1945 - 1965. Königswinter: EQIP Werbung & Verlag GmbH. pp. 25–26. ASIN B00LGYVJ4K.