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Shock and Vibration
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2021
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Article
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Tab 5
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Research Article
Experimental and Numerical Studies on Static Aeroelastic Behaviours of a Forward-Swept Wing Model
Table 5
The wing tip displacements when applying the aerodynamics of rigid wing (mm).
ā
Medium fidelity model
High fidelity model (CFD/CSD)
Linear
Nonlinear
LE point
34.74
34.65
34.59
TE point
29.10
29.03
29.10