To install click the Add extension button. That's it.

The source code for the WIKI 2 extension is being checked by specialists of the Mozilla Foundation, Google, and Apple. You could also do it yourself at any point in time.

4,5
Kelly Slayton
Congratulations on this excellent venture… what a great idea!
Alexander Grigorievskiy
I use WIKI 2 every day and almost forgot how the original Wikipedia looks like.
Live Statistics
English Articles
Improved in 24 Hours
Added in 24 Hours
Languages
Recent
Show all languages
What we do. Every page goes through several hundred of perfecting techniques; in live mode. Quite the same Wikipedia. Just better.
.
Leo
Newton
Brights
Milds

From Wikipedia, the free encyclopedia

X-112
Role Ground effect vehicle
National origin United States
Manufacturer Collins Radio Company
Designer Alexander Lippisch
First flight 1963
Number built 1
Developed into RFB X-113

The Collins X-112 was an experimental two-seat ground-effect vehicle, designed by Alexander Lippisch in the United States in the early 1960s to test his thick reverse delta wing concept.

YouTube Encyclopedic

  • 1/3
    Views:
    16 240
    48 656
    3 390
  • The Aerofoil Boat (undated)
  • Airfish-8 wing-in-ground effect vehicle by Wigetworks
  • Airfish 8

Transcription

Design and development

Lippisch's development of his Aerofoil Boat, a ground-effect vehicle for use over water, began whilst he was working in the aviation division of the Collins Radio Company in Cedar Rapids, Iowa, US. The Collins X-112 was built to test the concept.[1][2]

The Airfoil Boat was an inverse-delta aircraft, that is, it had a wing which was triangular in plan but with a straight, unswept leading edge.[1] Combined with strong anhedral, this layout produces stable flight in ground effect.[3] Specifically, it is claimed that it is stable in pitch and also that it can fly in ground effect at altitudes up to about 50% of its span, allowing it to operate over rough water. This contrasts with the lower-aspect-ratio square wing of the ekranoplans, which leaves ground effect at only 10% of span, limiting them to the calmer waters of lakes and rivers.[4]

Its fuselage was conventional, with flat sides and rounded decking. The nose-mounted single engine was of very low power, only 25 hp (19 kW). Two open cockpits were arranged in tandem, both over the wing. Aft of the trailing edge root the bottom of the fuselage rose strongly to carry a tall, broad fin and rudder. The X-112 had a T-tail, carrying elevators. Its thick airfoil wings were low-mounted, each with a tip float or "pontoon", which in combination with the strong anhedral kept the fuselage well clear of the water surface. Each float carried a winglet fitted with an aileron for roll control. A retractable water-rudder, fuselage-mounted at the point at which the lower fuselage rose upwards, provided directional control on the water surface.[1]

Tests made during 1963 began with the Airfoil Boat operated like any fast motor boat, planing on the surface. With speeds increased to around 36 mph (58 km/h) the X-112 rose clear of the surface as a ram-air air cushion or ground-effect vehicle. Solo free flights at up to 77 mph (124 km/h) were made; tests with two occupants were also conducted. "Entirely satisfactory" stability and control characteristics were reported under all these conditions.[1] With the Airfoil Boat proved, the X-112's mission was completed, and Lippisch, suffering from cancer, left Collins Radio. He recovered sufficiently to design and build its successor, the fibreglass, more powerful X-113 with Rhein-Flugzeugbau GmbH in Germany.[2]

Specifications

Data from Jane's All the World's Aircraft[1]

General characteristics

  • Crew: One or two
  • Length: 25 ft 0 in (7.62 m)
  • Wingspan: 14 ft 0 in (4.27 m)
  • Wing area: 110 sq ft (10 m2)
  • Empty weight: 370 lb (168 kg)
  • Gross weight: 710 lb (322 kg)
  • Powerplant: 1 × unknown, tractor configuration , 25 hp (19 kW)
  • Propellers: fixed pitch

Performance

  • Maximum speed: 77 mph (124 km/h, 67 kn) in free flight, flown solo
  • Take-off speed: 35—38 mph (55—61 km/h)

Sources

  • "The aerodynamics of the unconventional air vehicles of A. Lippisch", Henry V. Borst and Associates, 1980
  • US Patent 3190582 Ground Effect Aircraft with some X-112 characteristics [archive]
  • "The Aerofoil Boat X-112", Collins Video (https://www.youtube.com/watch?v=wlIK-xViG_4 [archive])

References

  1. ^ a b c d e Taylor, John W. R. (1964). Jane's All the World's Aircraft 1964–65. London: Sampson Low, Marston & Co. Ltd. p. 207.
  2. ^ a b Taylor, John W. R. (1974). Jane's All the World's Aircraft 1974–75. London: Jane's Yearbooks. p. 98. ISBN 0-354-00502-2.
  3. ^ Lee Qihui (2006). "Stability and Control of an Inverted Delta Wing In Ground Effect Aircraft" (PDF). Archived from the original (PDF) on June 22, 2007. Retrieved 25 September 2013.
  4. ^ "Ekratoplan vs. Lippisch". Archived from the original on 4 September 2013. Retrieved 25 September 2013.

External links

This page was last edited on 14 November 2022, at 13:35
Basis of this page is in Wikipedia. Text is available under the CC BY-SA 3.0 Unported License. Non-text media are available under their specified licenses. Wikipedia® is a registered trademark of the Wikimedia Foundation, Inc. WIKI 2 is an independent company and has no affiliation with Wikimedia Foundation.