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高超声速巡航飞行性能的优化分析
Alternative TitleOptimal analysis of hypersonic cruise flight performance
樊菁
Source Publication科学通报
2010-07-15
Volume55Issue:20Pages:1974-1979
ISSN0023-074X
Abstract高超声速巡航速度获得和维持都要消耗很多燃料,通过分析它们与飞行参数的关系,给出了高超声速巡航飞行的最佳速度.在相同飞行距离下,高超巡航飞行性能和最小能量弹道的比较表明,基于火箭动力的高超声速巡航导弹在现阶段很有竞争力
Keyword高超声速巡航 升阻比 最佳速度 广义有效载荷 发射质量
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Indexed ByCSCD
Language中文
Funding Organization国家自然科学基金委员会创新研究群体科学基金资助项目(10921062)
CSCD IDCSCD:4068465
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Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/43876
Collection高温气体动力学国家重点实验室
Corresponding Author樊菁
Recommended Citation
GB/T 7714
樊菁. 高超声速巡航飞行性能的优化分析[J]. 科学通报,2010,55(20):1974-1979.
APA 樊菁.(2010).高超声速巡航飞行性能的优化分析.科学通报,55(20),1974-1979.
MLA 樊菁."高超声速巡航飞行性能的优化分析".科学通报 55.20(2010):1974-1979.
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