Aerodynamic damping and stiffness determination for aircraft wing flutter speed analysis
The modeling of aircraft wing flutter using statically determined aerodynamic derivatives may not accurately represent the actual aeroelastic system. This paper presents an experimental method for estimating the transient aerodynamic derivatives relative to the airspeed for four 3D airfoil models. T...
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| Format: | Conference or Workshop Item |
| Published: |
2015
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| Subjects: |