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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2018
/
Article
/
Tab 1
/
Research Article
Static Aeroelastic Modeling and Rapid Analysis of Wings in Transonic Flow
Table 1
The parameter list of the model.
Model parameters
Data
Reference area (m
2
)
0.3926
Mean aerodynamic chord (m)
0.3445
Semispan (m)
1.2857