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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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力学所知识产出(19... [1]
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岳连捷 [3]
张新宇 [3]
肖雅斌 [3]
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Design methodology for shape transition inlets based on constant contraction of discrete streamtubes
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 卷号: 230, 期号: 8, 页码: 1496-1506
Authors:
Xiao YB(肖雅斌)
;
Yue LJ(岳连捷)
;
Ma SH
;
Zhang XY(张新宇)
;
Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100864, Peoples R China.
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View/Download:423/99
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Submit date:2016/09/14
Hypersonic Inlet
Shape Transition
Inward Turning
Scramjet
Design Method
污染组分对煤油燃料超燃冲压发动机性能影响分析
会议论文
高超声速研讨会暨第五届全国高超声速科学技术会议, 中国广西桂林, 2012-11-12
Authors:
万田
;
岳连捷
;
肖雅斌
;
仲峰泉
;
陈立红
;
张新宇
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Adobe PDF(58Kb)
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View/Download:545/138
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Submit date:2014/04/02
超燃冲压发动机
0煤油燃料
一维分析
发动机流场
等压比热
来流条件
组分
点火延迟时间
烧氢
实验台
热物理参数
正十烷
等熵分析
基元反应
气体参数
污染气体
影响因素分析
二维
污染空气
环己烷
带中心支板侧压进气道流场特性研究
期刊论文
实验流体力学, 2008, 卷号: 22, 期号: 1, 页码: 31-35
Authors:
龚鹏
;
岳连捷
;
肖雅斌
;
王世芬
;
张新宇
Adobe PDF(621Kb)
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View/Download:481/122
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Submit date:2010/05/03
超燃冲压发动机
高超声速进气道
侧压式进气道
支板