IMECH-IR  > 高温气体动力学国家重点实验室
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
URL查看原文
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
Citation statistics
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.
Files in This Item: Download All
File Name/Size DocType Version Access License
172.pdf(2305KB) 开放获取--View Download
Related Services
Recommend this item
Bookmark
Usage statistics
Export to Endnote
Google Scholar
Similar articles in Google Scholar
[樊菁]'s Articles
Baidu academic
Similar articles in Baidu academic
[樊菁]'s Articles
Bing Scholar
Similar articles in Bing Scholar
[樊菁]'s Articles
Terms of Use
No data!
Social Bookmark/Share
File name: 172.pdf
Format: Adobe PDF
This file does not support browsing at this time
All comments (0)
No comment.
 

Items in the repository are protected by copyright, with all rights reserved, unless otherwise indicated.