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大尺度空气舵超声速烧蚀热结构试验
引用本文:张友华%董永晖%陈连忠.大尺度空气舵超声速烧蚀热结构试验[J].宇航材料工艺,2008,38(5).
作者姓名:张友华%董永晖%陈连忠
作者单位:中国航天空气动力技术研究院,北京,100074
摘    要:针对全尺寸大尺度空气舵热环境参数,对地面试验的流场参数进行了计算,设计了测试探头,进行了流场校测。将校测结果与计算结果进行了比较分析,结果表明二者吻合较好,最大偏差在30%以内。校测后的流场已成功应用于试验。

关 键 词:大尺度空气舵  烧蚀热结构  流场

Ablation-Thermal-Structure Test of Large Scale Air Vane in Supersonic Flow
Zhang Youhua,Dong Yonghui,Chen Lianzhong.Ablation-Thermal-Structure Test of Large Scale Air Vane in Supersonic Flow[J].Aerospace Materials & Technology,2008,38(5).
Authors:Zhang Youhua  Dong Yonghui  Chen Lianzhong
Abstract:The ground test flow field parameters were computed based on the thermal conditions of the large full scale air vane. The test flow field parameters were also measured. The parameters computed accorded well with those measured. The maximum apparent error is below 30%.The flow field measured is used in tests successfully.
Keywords:Large scale air vane  Ablation-Thermal-Structure  Flow field
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