IMECH-IR  > 高温气体动力学国家重点实验室
复现高超声速飞行条件下10°尖锥标模气动力特性试验研究
刘云峰; 汪运鹏; 苑朝凯; 罗长童; 姜宗林
Source Publication中国力学大会-2015论文摘要集
2015
Conference Name中国力学大会-2015
Conference Date2015-08-16
Conference Place中国上海
Abstract综述了应用中科院力学所的JF12长试验时间激波风洞中,在复现40km高度,飞行马赫数7的试验条件下,开展的10°尖锥标模天平测力试验研究结果.
Keyword尖锥 标模 试验研究结果 气动力特性 激波风洞 力学所 试验条件 高超声速飞行 天平测力 飞行马赫数
DepartmentLHD激波与爆轰物理
Language中文
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/59290
Collection高温气体动力学国家重点实验室
Recommended Citation
GB/T 7714
刘云峰,汪运鹏,苑朝凯,等. 复现高超声速飞行条件下10°尖锥标模气动力特性试验研究[C],2015.
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