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Experimental Research on the Relationship Between SMA Wire Winding Angle and Torsional Actuator Perf
  • 所属机构名称：南京航空航天大学
  • 成果类型：会议
  • 相关项目：用于近空间飞行器仿生机翼的驱动器基础研究
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用于近空间飞行器仿生机翼的驱动器基础研究
期刊论文 21 会议论文 6
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