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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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Date Issued:2019
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Experimental and numerical investigation of the influence of roughness and turbulence on LUT airfoil performance
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1178-1190
Authors:
Li ST Li Y
;
Yang CX
;
Zheng XB
;
Wang Q
;
Wang Y
;
Li DS
;
Hu WR(胡文瑞)
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Submit date:2019/12/17
Airfoil
Dynamic load
Roughness
Vertical-axis wind turbines (VAWTs)
Wind tunnel experiment
Study of coupled effect of impingement jet cooling of kerosene with solid structure
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2019, 卷号: 62, 期号: 11, 页码: 2021-2028
Authors:
Du MM(杜蒙蒙)
;
Zhong FQ(仲峰泉)
;
Xing YF(邢云绯)
;
Zhang XY(张新宇)
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View/Download:388/99
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Submit date:2020/03/21
impingement jet cooling
hydrocarbon fuel
heat transfer enhancement
fluid-solid coupling
A nonlinear model for aerodynamic configuration of wake behind horizontal-axis wind turbine
期刊论文
APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2019, 卷号: 40, 期号: 9, 页码: 1313-1326
Authors:
Li DS
;
Guo T
;
Li RN
;
Yang CX
;
Cheng ZX
;
Li Y
;
Hu WR(胡文瑞)
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View/Download:186/74
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Submit date:2019/10/21
nonlinear wake aerodynamic model
vortex-induced velocity
integral equation of vortex-induced velocity
horizontal-axis wind turbine
O355
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:450/194
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Submit date:2020/03/21
Hypersonic vehicle
Six sigma robust optimization
Successive response surface
Thermal protection system
Uncertainty
Dynamic experimental studies of A6N01S-T5 aluminum alloy material and structure for high-speed trains
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 4, 页码: 763-772
Authors:
Liu ZS(刘子尚)
;
Yu YY
;
Yang Z(杨哲)
;
Wei YP(魏延鹏)
;
Cai JS
;
Li MH
;
Huang CG(黄晨光)
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Submit date:2019/10/14
Dynamic failure strain
Constitutive model
Dynamic mechanical properties
Deformation behavior of non-rigid airships in wind tunnel tests
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 3, 页码: 611-618
Authors:
Lu LL(路玲玲)
;
Song HW(宋宏伟)
;
Wang YW(王一伟)
;
Huang CG(黄晨光)
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View/Download:431/74
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Submit date:2019/01/09
Angle of attack
Fiber Bragg grating sensor
Flow velocity
Internal pressure
Non-rigid airship
Wind tunnel test