High-resolution simulation for rotorcraft aerodynamics in hovering and vertical descending flight using a hybrid method
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This work was co-supported by the Funding of Jiangsu Innovation Program for Graduate Education of ChinaKYLX16_0389;the Fundamental Research Funds for the Central Universities of China
2018-06-20(万方平台首次上网日期,不代表论文的发表时间)
共13页
1053-1065