IMECH-IR  > 高温气体动力学国家重点实验室
Shape Optimization for Hypersonic Arc-Wing Missiles
Cui K(崔凯); Yang GW(杨国伟)
Source PublicationJournal of Spacecraft and Rockets
2010
Volume47Issue:4Pages:694-700
ISSN0022-4650
DOI10.2514/1.45882
Indexed BySCI
Language英语
WOS IDWOS:000281019200018
WOS KeywordMULTIDISCIPLINARY DESIGN OPTIMIZATION ; CONICAL FLOWFIELDS ; GENETIC-ALGORITHM ; PERFORMANCE
WOS Research AreaEngineering
WOS SubjectEngineering, Aerospace
Funding OrganizationNational Natural Science Foundation of China (NO.90916013)
Citation statistics
Cited Times:7[WOS]   [WOS Record]     [Related Records in WOS]
Document Type期刊论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/42436
Collection高温气体动力学国家重点实验室
Corresponding AuthorCui K(崔凯)
Recommended Citation
GB/T 7714
Cui K,Yang GW. Shape Optimization for Hypersonic Arc-Wing Missiles[J]. Journal of Spacecraft and Rockets,2010,47(4):694-700.
APA 崔凯,&杨国伟.(2010).Shape Optimization for Hypersonic Arc-Wing Missiles.Journal of Spacecraft and Rockets,47(4),694-700.
MLA 崔凯,et al."Shape Optimization for Hypersonic Arc-Wing Missiles".Journal of Spacecraft and Rockets 47.4(2010):694-700.
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