Gust Response Analysis for Helicopter Rotors in the Hover and Forward Flights
Dynamic load due to gust for helicopter rotors directly affects the structural stress and flight performance. In case of gust, it may cause the loss of trust force or the increase of deflection for rotors. In current work, an effective coupled aeroelastic model based on a medium-deflection beam theo...
Збережено в:
| Автори: | , , |
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| Формат: | Artigo |
| Мова: | Inglês |
| Опубліковано: |
Wiley
2017-01-01
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| Серія: | Shock and Vibration |
| Онлайн доступ: | http://dx.doi.org/10.1155/2017/8986217 |
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