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SHAN Xiaowen
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Journal article
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2025
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Aerodynamic optimization
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Multi-fidelity model
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Propeller noise
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Tilt rotor
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VTOL
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Aerospace Science and Techn...
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Design approach for tilt propellers of UAM/eVTOLs for cruise and hover considering aerodynamic and aeroacoustic characteristics via a multi-fidelity model
Journal article
Aerospace Science and Technology,2025, volume: 156
Authors:
Ye, Yingzhe
;
Liang, Yu
;
Shan, Xiaowen
;
Huang, Kefu
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Submit date：2025/03/10
Aerodynamic optimization
Multi-fidelity model
Propeller noise
Tilt rotor
VTOL
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