CFD simulation of helicopter rotor flow based on unsteady actuator disk model
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This study was co-supported by the grant 'State task of the Education and Science Ministry of Russian Federation"agree-ment No. 075-03-2020-051/3 from 09.06.2020. theme No. fzsu-2020-0021
2020-09-29(万方平台首次上网日期,不代表论文的发表时间)
共16页
2313-2328