Static Aeroelastic Modeling and Rapid Analysis of Wings in Transonic Flow

Table 7

The comparison of the displacement of the wing tip by the CFD/CSD method and modeling method.

Dynamic pressure (Pa)	LE_CFD (m)	LE_model (m)	LE_error	TE_CFD (m)	TE_model (m)	TE_error
20,000	0.006859	0.006994	+1.96%	0.007617	0.007609	−0.10%
40,055.4	0.01313	0.01335	+1.70%	0.01468	0.01471	+0.20%
50,000	0.01635	0.01655	+1.20%	0.01792	0.01809	+0.95%
60,000	0.01932	0.01949	+0.85%	0.02112	0.02114	+0.10%
80,000	0.02480	0.02497	+0.72%	0.02727	0.02725	−0.06%