Cierva C.3
C.3 | |
---|---|
Role | experimental autogyro Type of aircraft |
Manufacturer | Juan de la Cierva |
Designer | Juan de la Cierva |
Number built | 1 |
The Cierva C.3 was an experimental autogyro built by Juan de la Cierva in Spain in 1921.[citation needed] It was based on the fuselage of a Sommer monoplane, and was actually completed and tested before that aircraft. The C.3 utilised a single, three-bladed rotor in place of the coaxial double rotor tested on the C.1. A few short hops were achieved in testing and Cierva noted a tendency for the machine to want to roll over, thus alerting him to the problem of dissymmetry of lift that he would have to overcome in order to build a successful rotary-wing aircraft. The C.3 was damaged and rebuilt four times before being abandoned without having flown, la Cierva returning to work on the C.2.
References
- Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 254.
- World Aircraft Information Files. London: Bright Star Publishing. pp. File 891 Sheet 28.
- Leishman, J. Gordon (2006). Principles of Helicopter Aerodynamics. Cambridge: Cambridge University Press. p. 699.
See also
- v
- t
- e
Cierva aircraft
- C.1
- C.2
- C.3
- C.4
- C.5
- C.6
- C.7
- W.4
- W.5
- W.6
- W.9
- W.11 Air Horse
- W.14 Skeeter