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Ryan YO-51 Dragonfly

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YO-51 Dragonfly
Role Army observation and liaison
Manufacturer Ryan Aeronautical
First flight 1940
Primary user United States Army Air Corps
Number built 3

TheRyan YO-51 Dragonflywas anobservation aircraftdesigned and built byRyan Aeronauticalfor theUnited States Army Air Corps(USAAC). A single-enginedparasol wingmonoplane,it was designed for optimumSTOLcapability, but although three prototypes proved highly successful in testing, theStinson YO-49was judged superior and no production contract was placed.

Design

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The design of the YO-51 Dragonfly was typical for aircraft of its type, being optimised for the observation and liaison role, with emphasis on the ability to operate out of the smallest possible airfields.[1]The Dragonfly was a high-wing bracedparasolmonoplanewith fixed tailwheellanding gear,a two-seat open cockpit, and full-spanslotsandFowler flapsforSTOLcapability.[2]It was powered by a singlePratt & Whitney R-985-21 Wasp Juniorradial engine.[3]

At gross weight, the YO-51 could, without flaps, take off after a run of 400 feet, while with full flaps the takeoff run would be only 75 feet, or just four feet more than twice its own length.[4]The Dragonfly was capable of maintaining level flight at speeds as low as 30 miles per hour (48 km/h),[5]and was claimed as being capable of landing in a distance shorter than the length of the aircraft itself.[6]

Operational history

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Nicknamed the "flying motorcycle",[7]three YO-51 aircraft were acquired by the United States Army Air Corps to take part in afly-offevaluation against theStinson YO-49andBellanca YO-50to supply a new observation and liaison aircraft for use by the USAAC.[8]The YO-51 was the heaviest of the three aircraft evaluated.[9]

Although the Dragonfly was considered satisfactory during its flight testing,[10]conducted atWright Fieldin Ohio,[11]the Stinson machine won the production contract, and no further YO-51s were built.[12]

Specifications

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YO-51 on the ground

Data fromDonald 1997[3]

General characteristics

  • Crew:two (pilot and observer)
  • Length:35 ft 6 in (10.82 m)
  • Wingspan:52 ft (16 m)
  • Height:11 ft 1 in (3.38 m)
  • Gross weight:4,206 lb (1,908 kg)
  • Powerplant:1 ×Pratt & Whitney R-985-21 Wasp Juniorradial,440 hp (330 kW)

Performance

  • Maximum speed:129 mph (208 km/h, 112 kn)
  • Cruise speed:107 mph (172 km/h, 93 kn)
  • Stall speed:30 mph (48 km/h, 26 kn)

Armament

  • None

See also

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Aircraft of comparable role, configuration, and era

Related lists

References

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Notes
  1. ^Penfield 1941, p.31.
  2. ^Foottit, H. R. (February 1942). "The Fowler Flap".Flying and Popular Aviation.30(2). Chicago: Ziff-Davis Publishing Co.: 71.
  3. ^abDonald 1997, p.794.
  4. ^Fowler 1948, p.79.
  5. ^Rowe 2006, p.22.
  6. ^Wilson, Gill Robb (July 1954). "Genealogy of American Aircraft".Flying.55(1). Chicago: Ziff-Davis Publishing Co.: 23.
  7. ^"U. S. Army's" Flying Motorcycle "".The Boston Globe.Boston, MA. May 25, 1941. p. C1.
  8. ^Pattillo 2001, p.137.
  9. ^Adcock 2005, p.5.
  10. ^"The Dragonfly---Army's Newest Observation Plane".The Milwaukee Sentinel.Milwaukee, WI. February 23, 1940. p. 2.
  11. ^"Army Tests New B-17C".The New York Times.New York. November 17, 1940.Retrieved2012-08-11.
  12. ^Merriam 2002, p.26.
Bibliography
  • Adcock, Al (2005).US Liaison Aircraft in action.Aircraft in Action. Vol. 195. Carrollton, TX: Squadron/Signal Publications.ISBN978-0897474870.
  • Donald, David (1997).Complete Encyclopedia of World Aircraft.London: Orbis Publishing Ltd.ISBN0760705925.
  • Fowler, Harlan Davey (1948).Fowler Flaps for Airplanes: An engineering handbook.Los Angeles: Wetzel Publishing Co.ASINB0007EA17Q.
  • Merriam, Ray, ed. (2002).World War II Journal #15: U.S. Military Aircraft of World War II.Bennington, VT: Merriam Press.ISBN1576381676.
  • Pattillo, Donald M. (2001).Pushing the Envelope: The American Aircraft Industry.Ann Arbor, MI: University of Michigan Press.ISBN978-0472086719.
  • Penfield, Thomas (1941).Wings for America: Fighting Planes of the U. S. A.Chicago: Rand McNally & Co.ASINB004BVUSC4.
  • Rowe, Frank Joseph (2006).The Helio Courier Ultra C/stol Aircraft: An Illustrated Developmental History.Jefferson, NC: McFarland & Company.ISBN978-0786422890.
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