A wind-tunnel based study of helicopter tail rotor blade vortex interaction
The interaction of a helicopter tail rotor blade with the tip vortex system from the main rotor is a significant source of noise and, in some flight states, can produce marked reductions in control effectiveness. This paper describes a series of wind-tunnel tests to simulate tail rotor blade vortex...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
2004-05.
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| Subjects: | |
| Online Access: | Get fulltext |