pCRM9 aeroelastic aircraft wing model for NASTRAN

This is the pCRM9 aeroelastic finite element model. It is based on the University of Michigan undeflected CRM geometry (uCRM). This FEM model is tailored for optimisation and load analysis using NASTRAN.本数据集为pCRM9气动弹性有限元模型。其基于密歇根大学（University of Michigan）的无变形CRM几何构型（uCRM）。该有限元模型专为使用NASTRAN进行优化与载荷分析而定制。