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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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State Key ... [6]
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吴振杰 [2]
岳连捷 [2]
崔凯 [2]
张启帆 [2]
王秀平 [2]
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11902325) [1]
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双排凹腔燃烧室释热区转移过程中的特性研究
期刊论文
推进技术, 2023, 页码: 13
Authors:
吴振杰
;
张启帆
;
罗苇航
;
高占彪
;
岳连捷
Adobe PDF(1258Kb)
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View/Download:85/21
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Submit date:2023/05/08
双排凹腔
燃烧室
稳焰
超声速燃烧
火焰不对称
Experimental study of hysteresis and catastrophe in a cavity-based scramjet combustor
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 10, 页码: 118-133
Authors:
Zhang X(张旭)
;
Zhang QF(张启帆)
;
Wu ZJ(吴振杰)
;
Yue LJ(岳连捷)
;
Gao ZB(高占彪)
;
Luo WH(罗苇航)
;
Chen H(陈昊)
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View/Download:23/0
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Submit date:2023/07/17
Catastrophe
Cavity-based scramjet
Flame stabilization
Flame/shock interaction
Hysteresis
高超声速飞行器上壁面多目标优化及性能分析
期刊论文
力学学报, 2013, 卷号: 45, 期号: 2, 页码: 193-201
Authors:
高太元
;
崔凯
;
胡守超
;
王秀平
Adobe PDF(3380Kb)
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Submit date:2013/04/07
高超声速
遗传算法
机体容积
升阻比
计算流体力学
Analysis and application of high resolution numerical perturbation algorithm for Convective-Diffusion Equation
期刊论文
Chinese Physics Letters, 2012, 卷号: 29, 期号: 10, 页码: 104702
Authors:
Gao Z(高智)
;
Shen YQ(申义庆)
Adobe PDF(1310Kb)
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Submit date:2012/12/04
三维后体/尾喷管一体化构型优化设计及性能分析
期刊论文
科学通报, 2012, 卷号: 57, 期号: 4, 页码: 239-247
Authors:
高太元
;
崔凯
;
王秀平
;
胡守超
;
杨国伟
;
任亮
Adobe PDF(2922Kb)
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View/Download:946/200
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Submit date:2013/01/16
高超声速
后体/尾喷管一体化
单壁扩张喷管
优化设计
计算流体动力学
Acoustic Calculation for Supersonic Turbulent Boundary Layer Flow
期刊论文
Chinese Physics Letters, 2009, 卷号: 26, 期号: 9, 页码: 094701-1-4
Authors:
Li XL(李新亮)
;
Fu DX(傅德薰)
;
Ma YW(马延文)
;
Gao H(高慧)
Adobe PDF(1149Kb)
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Submit date:2010/03/07
Direct Numerical-simulation
Sound