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- W2349096221 abstract "The aerodynamic performance and flying safety of HALE(High Altitude and Long Endurance) UAVs are largely affected by the aeroelastic distortion of its large aspect ratio wing.Large aspect ratio wing of UAV is bended and twisted by the air load during flight and thus is not to be treated as a traditional rigid wing.The effect of static aeroelastic distortion to the aeroelasticity for a large aspect ratio wing under different load statuses is analyzed.The integrated design method combining aerodynamics with structural dynamics is adopted in this analysis using computational fluid dynamics(CFD) program CFX and computational structual dynamics(CSD) program ANSYS.The results show that the local angle of attack changs with reduced lift and increased drag of the aeroelastic wing and the wingtip is liable to stall." @default.
- W2349096221 created "2016-06-24" @default.
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- W2349096221 date "2012-01-01" @default.
- W2349096221 modified "2023-09-27" @default.
- W2349096221 title "CFD/CSD-based aeroelastic analysis of large aspect ratio wing" @default.
- W2349096221 hasPublicationYear "2012" @default.
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