Research Article

Efficient Method for Aeroelastic Tailoring of Composite Wing to Minimize Gust Response

Table 2

CPU time distribution in optimization process.

Time distributionQ-static methodDynamic responseOther calculation

Time for a cycle1.922 s81.03 s0.79 s
Total cycles1006100
Total time used192.2 s486.2 s79.0 s
Share of time25.4%64.2%10.4%