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Indexed By:SCI
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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Theories and methods for designing hypersonic high-enthalpy flow nozzles
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339
Authors:
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
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View/Download:177/44
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Submit date:2022/06/10
Boundary layer correction
High-enthalpy flow
Hypersonic wind tunnel
Nozzle design
Real-gas effects
Parameters for evaluating the efficiency of inlet compression
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
Authors:
Chen KT(陈科挺)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(511Kb)
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View/Download:236/53
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Submit date:2022/01/12
Airbreathing engine
Compression efficiency
Compression quality
Inlet
Self-consistency
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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Submit date:2021/03/30
High-enthalpy flow
Hypersonic wind tunnel
Aerospace vehicle
Aerodynamic balance
Heat flux sensor
Optical measurement technique
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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View/Download:904/301
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Submit date:2013/09/21
Baldwin-lomax Model
Boundary Layers
Computational Aerodynamics
Entropy
Supersonic Flows
Turbulence Models