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岳连捷 [2]
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Source Publication：AEROSPACE SCIENCE AND TECHNOLOGY
Funding Project：National Natural Science Foundation of China[11472279]
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Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors:
Tong XT(仝晓通)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(8067Kb)
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View/Download：399/69
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Submit date：2021/03/03
Unsteady pressure measurement
Pressure sensor
Pressure transmission tube
Dynamic response
Compressible flow
Numerical study of a fully confined supersonic slot impinging jet from bleed system
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Chang XY(张新宇)
Adobe PDF(3918Kb)
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View/Download：539/173
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Submit date：2019/09/09
Fully confined supersonic jet
Inclined impingement
Heat transfer
Boundary layer bleed
Numerical simulation
