Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings
Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings
复制标题
用于研究跨音速飞机机翼的基准航空结构模型
作者：
Timothy R. Brooks;G. Kenway;J. Martins
自引入以来，NASA共同研究模型已被证明是一个有用的空气动力学基准，用于预测基于计算流体动力学的阻力和气动设计优化。模式..。
Since its introduction, the NASA Common Research Model has proved a useful aerodynamic benchmark for predicting computational-fluid-dynamics-based drag and aerodynamic design optimization. The mode...