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Knowledge Management System of Institue of Mechanics, CAS
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姜宗林 [2]
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Indexed By:CSCD
Indexed By:EI
Source Publication:CHINESE JOURNAL OF AERONAUTICS
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Criteria for hypersonic airbreathing propulsion and its experimental verification
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:
Jiang ZL(姜宗林)
;
Zhang ZJ(张子健)
;
Liu YF(刘云峰)
;
Wang C(王春)
;
Luo ZT(罗长童)
Adobe PDF(1806Kb)
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Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Ma SH(马生虎)
;
Zhang QF(张启帆)
;
Zhang, Peng
;
Zhang XY(张新宇)
Adobe PDF(3937Kb)
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Submit date:2021/03/30
Adverse pressure gradient
Back pressure
Hysteresis effects
Non-uniform flow
Shock train
Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475
Authors:
Wang Q(汪球)
;
Luo K(罗凯)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
Adobe PDF(2057Kb)
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Submit date:2020/08/26
Shock tunnel
Detonation driver
Diaphragm
Dual ignition
High-enthalpy flow
Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108
Authors:
Zhu JJ
;
Wang XJ
;
Zhang HG
;
Li YW
;
Wang RX(王睿星)
;
Qiu ZP
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View/Download:452/194
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Submit date:2020/03/21
Hypersonic vehicle
Six sigma robust optimization
Successive response surface
Thermal protection system
Uncertainty
Shock/shock interactions between bodies and wings
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 2, 页码: 255-261
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Teng HH(腾宏辉)
;
Jiang ZL(姜宗林)
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Submit date:2018/10/30
Body And Wing
Flow Field
Hypersonic Flow
Shock/shock Interaction
Wave Configurations
Numerical studies of static aeroelastic effects on grid fin aerodynamic performances
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2017, 卷号: 30, 期号: 4, 页码: 1300-1314
Authors:
Huang CD(黄程德)
;
Liu W(刘文)
;
Yang GW(杨国伟)
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View/Download:346/102
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Submit date:2017/11/29
Aeroelasticity
Fluid-structure Interpolation
Grid Fin
Mesh Deformation
Radial Basis Function
A quasi-one-dimensional model for hypersonic reactive flow along the stagnation streamline
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2016, 卷号: 29, 期号: 6, 页码: 1517-1526
Authors:
Chen S
;
Sun QH(孙泉华)
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View/Download:269/73
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Submit date:2017/04/26