Static Aeroelastic Modeling and Rapid Analysis of Wings in Transonic Flow

Table 6

The comparison of the deflection results of the reference and experimental data.

Reference result		Computational result		Experimental data
LE_deflection (m)	TE_deflection (m)	LE_deflection (m)	TE_deflection (m)	Wing tip deflection (m)
0.01289	0.01374	0.01372	0.01467	0.01250