- The tail boom strake and helicopter yaw control
Article
CID:
- 14132
Authors:
- Adams, M.
- Newman, S.
Publication Date:
- 2004
Issue Date:
- 2004
Journal Title:
- Aircraft Engineering and Aerospace Technology
Issue No.:
- 76
Issue number:
- 2
Collation:
- 143-159
Subjects:
- Helicopter Aerodynamics
Fiction:
- 0
Notes:
- (GEN) Describes the pedal travel behaviour caused by aerodynamic interaction between the main rotor wake, the sideways velocity and subsequent forces generated by the tail boom noticed in Sea King helicopters operating under extreme conditions during the Falklands conflict.