Aerodynamic forces; 2D morphing - numerical simulations - incidence 1.8 deg - static case
收藏DataCite Commons2021-04-15 更新2025-04-09 收录
下载链接：
https://dataverse.callisto.calmip.univ-toulouse.fr/citation?persistentId=doi:10.48531/JBRU.CALMIP/BUABFJ
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资源简介：
ASCII file containing aerodynamic forces around an A320 wing. From a 2D numerical simulation performed with the NSMB code. The first four columns give the physical time in seconds, the drag coefficient, the lift coefficient and the pitching moment coefficient for a morphing wing. The trailing edge not vibrating, it is the so-called static case.
提供机构：
Root
创建时间：
2021-04-02
