Static Aeroelastic Modeling and Rapid Analysis of Wings in Transonic Flow

Table 4

The grid information.

Grid information parameters	Data
Viscous wall spacing (m)	1.0 × 10^−5
Growth rate of the boundary layer	1.3
Prism layer cells	20
Surface mesh size (elements)	47,176
Surface mesh size (nodes)	23,679
Grid size (elements)	1,484,903
Grid size (nodes)	577,111