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Aeroelastic analysis of a non-linear airfoil based on unsteady vortex lattice model
Y. H. Zhao
*
,
H. Y. Hu
*
Corresponding author for this work
Nanjing University of Aeronautics and Astronautics
Research output
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Article
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peer-review
48
Citations (Scopus)
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Engineering
Vortex
100%
Aerodynamic Model
100%
Airfoil
100%
Airfoil Section
40%
Time Domain
20%
Nonlinearity
20%
Continuous Time
20%
Discrete Time
20%
Two Dimensional
20%
Reduced Order Model
20%
Limit Cycle
20%
Eigenmode
20%
Dimensionless Form
20%
Aeroelastic Behavior
20%
Theodorsen
20%
Physics
Airfoil
100%
Airfoil Profiles
100%
Statics
50%