Skip to main content

The Gyrodyne—A Forgotten High Performer?

Buy Article:

$22.00 plus tax (Refund Policy)

The Gyrodyne was a high‐performance rotorcraft concept developed by the Fairey Aviation Company in the 1940's. The aircraft achieved the world helicopter speed record of 129 mph in the G class in 1948. It was, and is, unique in that it featured a propeller offset from the centerline of the aircraft, thereby fulfilling the dual role of anti‐torque device and auxiliary propulsion. This paper examines the flight mechanics and performance aspects of a configuration that appears not to have found favor in subsequent compound helicopter concepts. Design compromises in the implementation of a propeller or rotor for combined anti‐torque and propulsion requirements are discussed qualitatively. A contemporary rotorcraft flight mechanics simulation model is then used to quantitatively examine the trim, stability, control response and performance differences between a conventional medium single main and tail rotor helicopter, and a potential gyrodyne equivalent. The results suggest that the gyrodyne can achieve a maximum speed, limited by retreating blade stall, that is 30% higher than the equivalent helicopter. However, power requirements at hover and low speed are some 10% greater, and lateral/directional stability and response characteristics are poorer. Notwithstanding this it is concluded that the gyrodyne concept offers an elegant and efficacious design solution to the high performance helicopter problem.
No Reference information available - sign in for access.
No Citation information available - sign in for access.
No Supplementary Data.
No Data/Media
No Metrics

Document Type: Research Article

Affiliations: Department of Aerospace Engineering, University of Glasgow, Glasgow, UK

Publication date: 2007-10-01

More about this publication?
  • The Journal of the American Helicopter Society is the world's only scientific journal dedicated to vertical flight technology. It is a peer-reviewed technical journal published quarterly by AHS International and presents innovative papers covering the state-of-the-art in all disciplines of rotorcraft design, research and development. (Please note that AHS members receive significant discounts on articles and subscriptions.)

    Journal subscribers who are AHS members log in here if you are not already logged in.

    Authors can find submission guidelines and related information on the AHS website.

  • Access Key
  • Free content
  • Partial Free content
  • New content
  • Open access content
  • Partial Open access content
  • Subscribed content
  • Partial Subscribed content
  • Free trial content
Cookie Policy
Cookie Policy
Ingenta Connect website makes use of cookies so as to keep track of data that you have filled in. I am Happy with this Find out more