Numerical optimization of helicopter rotor blade design for active twist control
The vibration of a helicopter has several different sources, such as the rotor, engine and transmission system. This creates a number of problems with performance, for example poor manoeuvrability, discomfort of the pilot, low fatigue life of the structural components, and, consequently, high opera...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Vilnius Gediminas Technical University
2007-09-01
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| Series: | Aviation |
| Subjects: | |
| Online Access: | https://bjrbe.vgtu.lt/index.php/Aviation/article/view/7039 |