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Force measurement using strain-gauge balance in shock tunnel based on deep learning
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 8, 页码: 43-53
Authors:
Nie SJ(聂少军)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
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Submit date:2024/02/26
Convolutional neural net-works
Deep learning
Frequency domain analysis
Force measurement
Time domain analysis
Recurrent neural networks
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel
期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(2434Kb)
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View/Download:346/99
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Submit date:2022/08/23
Aerodynamic Coefficients
Two Stage to Orbit
Aerodynamic Performance
Hypersonic Flight
Hypersonic Wind Tunnels
Solenoid Valves
Oblique Shock
Pneumatic Actuator
Hypersonic Flows
Computer Aided Engineering
Experimental Study of Kerosene Ignition and Flame Stabilization in a Supersonic Combustor
期刊论文
International Journal of Turbo & Jet-Engines, 2022, 卷号: 39, 期号: 3, 页码: 403-410
Authors:
Meng Y(孟宇)
;
Gu HB(顾洪斌)
;
Zhang XY(张新宇)
Adobe PDF(3187Kb)
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Submit date:2021/10/29
Design of a milli-newton force balance for hypersonic rarefied wind tunnel
期刊论文
MEASUREMENT, 2021, 卷号: 185, 页码: 7
Authors:
Wu CW(吴臣武)
;
Liu C(刘聪)
;
Hu DL(胡灯亮)
;
Liu HL(刘宏立)
;
Huang HJ(黄河激)
Adobe PDF(4178Kb)
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Submit date:2021/11/15
Strain
Balance
Milli-newton
Design
Calibration
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
Authors:
Li, Mengzhe
;
Wang, Zhikai
;
Xu, Rongguang
;
Zhang, Xiaoliang
;
Chen, Zhitong
;
Wang Q(汪球)
Adobe PDF(8841Kb)
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Submit date:2021/11/01
Non-equilibrium plasma
Plasma-assisted ignition
Plasma-assisted combustion
Aerospace engine
Combustor
Extreme condition
Atomization of misaligned impinging liquid jets
期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 9, 页码: 15
Authors:
Zhang, Chenwei
;
Zhang ZY(张振宇)
;
Wu K(吴坤)
;
Xia, Xi
;
Fan XJ(范学军)
Adobe PDF(15401Kb)
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Submit date:2022/01/12
AMP Exception
AMP Exception
Theoretical, numerical and experimental study of hypersonic boundary layer transition: Blunt circular cone
期刊论文
APPLIED THERMAL ENGINEERING, 2021, 卷号: 194, 页码: 14
Authors:
Chen, Jianqiang
;
Yi, Shihe
;
Li XL(李新亮)
;
Han GL(韩桂来)
;
Zhang, Yifeng
;
Yang, Qiang
;
Yuan, Xianxu
Adobe PDF(11175Kb)
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Submit date:2021/08/03
Hypersonic boundary layer
Stability
Transition
Thermal protection
Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 12
Authors:
Yuan CK(苑朝凯)
;
Jiang ZL(姜宗林)
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Submit date:2021/03/03
Hypersonics
Shock tunnels
Flow characteristics
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
Synthesis and characterization of light-weight porous ceramics used in the transpiration cooling
期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 177, 页码: 438-445
Authors:
Zhang, Bo
;
Huang, Jie
;
Li, Weijie
;
Huang, Haiming
;
Zhao, Huanyu
;
Peng JL(彭锦龙)
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Submit date:2021/03/30
Carbon fiber-reinforced silicon carbide porous ceramics
Permeability
Oxyacetylene flame test
Transpiration cooling