Multibody Simulation of Helicopter Rotor with Structural Flexibility

Date

2019-10-30

Author

Turan, Bali İhsan
Kayran, Altan

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URI

https://hdl.handle.net/11511/75859

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Multibody simulation of helicopter rotor with structural flexibility Özturan, Bali İhsan; Kayran, Altan; Department of Aerospace Engineering (2019) Most of the multibody simulation tools used for modeling helicopter rotor use beam models of the blade and the rigid rotor hub. Stress recovery in the blade and in the hub are then performed by means of cross-sectional analysis tools or finite element analysis tools. In this study, multibody model of a helicopter main rotor is established using three dimensional flexible models of the blade and the rotor hub, and multibody simulations of the rotor are performed for the hover and the forward flight load case...
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Citation Formats

B. İ. Turan and A. Kayran, “Multibody Simulation of Helicopter Rotor with Structural Flexibility,” 2019, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/75859.