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.<br>

本数据集为pCRM9气动弹性有限元模型（aeroelastic finite element model）。该模型基于密歇根大学未变形CRM几何构型（uCRM）。此有限元模型专为使用NASTRAN开展优化设计与载荷分析而定制。