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 modelHigh fidelity model (CFD/CSD)
LinearNonlinear

LE point34.7434.6534.59
TE point29.1029.0329.10