Home  

Random  

Nearby  



Log in  



Settings  



Donate  



About Wikipedia  

Disclaimers  



Wikipedia





Cierva C.29





Article  

Talk  



Language  

Watch  

Edit  





The Cierva C.29 was a five-seat British cabin autogyro built in 1934 as a joint venture between Westland Aircraft and Cierva.[1] The rotor system and rotors were designed by Cierva and the fuselage by Westland. It was powered by a 600 hp (447 kW) Armstrong Siddeley Panther II engine with a two-bladed tractor propeller; the engine also drove the three-bladed rotor via a clutched shaft. The C.29 suffered from ground resonance during ground running and was not flown.[1] It was later acquired for evaluation by the Royal Aircraft Establishment but it was unable to cure the resonance problem and the autogyro was scrapped in 1939.

C.29
Role Five-seat cabin autogyro
National origin United Kingdom
Manufacturer Cierva
Produced 1934
Number built 1

Specifications

edit

Data from Aircraft Data Sheet: Cierva C-29 (1934)][1]

General characteristics

Performance

References

edit

Notes

edit
  • ^ a b James 1991, p. 226.
  • Bibliography

    edit
    edit

    Retrieved from "https://en.wikipedia.org/w/index.php?title=Cierva_C.29&oldid=1003733322"
     



    Last edited on 30 January 2021, at 11:58  





    Languages

     


    Deutsch
    Тоҷикӣ
     

    Wikipedia


    This page was last edited on 30 January 2021, at 11:58 (UTC).

    Content is available under CC BY-SA 4.0 unless otherwise noted.



    Privacy policy

    About Wikipedia

    Disclaimers

    Contact Wikipedia

    Code of Conduct

    Developers

    Statistics

    Cookie statement

    Terms of Use

    Desktop