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Indexed By:EI
Source Publication:CHINESE JOURNAL OF AERONAUTICS
Community:高温气体动力学国家重点实验室
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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
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:
Jiang ZL(姜宗林)
;
Hu ZM(胡宗民)
;
Wang YP(汪运鹏)
;
Han GL(韩桂来)
Adobe PDF(1129Kb)
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View/Download:349/177
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Submit date:2021/03/30
High-enthalpy flow
Hypersonic wind tunnel
Aerospace vehicle
Aerodynamic balance
Heat flux sensor
Optical measurement technique
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
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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Submit date:2017/04/26
Improvement of Baldwin-Lomax turbulence model for supersonic complex flows
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 期号: 3, 页码: 529–534
Authors:
Zhao R(赵瑞)
;
Yan C(阎超)
;
Yu J(于剑)
;
Li XL(李新亮)
;
Yan, C (reprint author), Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China.
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Submit date:2013/09/21
Baldwin-lomax Model
Boundary Layers
Computational Aerodynamics
Entropy
Supersonic Flows
Turbulence Models