摘要: The most common rocket nozzle has an axisymmetric, convergent-divergent shape. Advanced rocket motor nozzles aspire to improve the rocket motor performance by various means or nozzles of non-conventional geometries. An experimenta... 展开
作者 | Lior Miller Savely Khosid Benveniste Natan | ||
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作者单位 | |||
文集名称 | 58th Israel annual conference on aerospace 2018 | ||
出版年 | 2018 | ||
出版社/出版地 | Department of Aerospace Technology / Haifa | ||
会议名称 | Israel Annual Conference on Aerospace Sciences | ||
开始页/总页数 | 880 / 15 | ||
会议日期/会议地点 | 20180314-15 / Haifa | 会议年/会议届次 | 2018 / 58th |
中图分类号 | V4 | ||
馆藏号 | N2018091200178841 |