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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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姜宗林 [5]
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罗长童 [3]
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Data-driven rapid prediction model for aerodynamic force of high-speed train with arbitrary streamlined head
期刊论文
ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS, 2022, 卷号: 16, 期号: 1, 页码: 2190-2205./通讯作者:Sun, Zhenxu
Authors:
Chen, Dawei
;
Sun ZX(孙振旭)
;
Yao, Shuanbao
;
Xu SF(许盛峰)
;
Yin B(银波)
;
Guo DL(郭迪龙)
;
Yang GW(杨国伟)
;
Ding, Sansan
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Submit date:2022/12/20
Aerodynamic force
inverse design
high-speed train
SVM
numerical simulation
wind tunnel test
Study on Aerodynamic Performance of Maglev Train Passing by Each Other at Constant Speed
期刊论文
力学研究, 2021, 期号: 2
Authors:
Yu M(于淼)
;
Zhu BN(祝百年)
;
Liang YT(梁永廷)
;
Hao ZZ(郝占宙)
;
Yin B(银波)
Adobe PDF(1196Kb)
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Submit date:2022/03/16
磁悬浮列车
列车交会
气动力
气动升力
振荡
Maglev Train
Train Passing by Each Other
Aerodynamic Force
Aerodynamic Lift
Oscillation
Impulse force-measurement system
期刊论文
SHOCK WAVES, 2020, 页码: 11./通讯作者:Wang, Y.
Authors:
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
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Submit date:2020/11/30
Shock tunnel
High enthalpy
Aerodynamic force measurement
Strain gauge balance
Weighting by Cross-Validation: A Calibration Method for Force Measurements via Transient Response Analysis
期刊论文
EXPERIMENTAL TECHNIQUES, 2019, 卷号: 43, 期号: 4, 页码: 469-478./通讯作者:Luo, C.
Authors:
Luo ZT(罗长童)
;
Wang YP(汪运鹏)
;
Hu ZM(胡宗民)
;
Li JP(李进平)
;
Jiang ZL(姜宗林)
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Submit date:2019/10/21
Aerodynamic force measurement
Dynamic system
Impact response
Cross-validation
System identification
高速列车受电弓平台的优化设计
期刊论文
力学研究, 2018, 卷号: 7, 期号: 2, 页码: 27-35
Authors:
林鹏
;
张业
;
郭迪龙
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View/Download:365/89
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Submit date:2018/12/13
[7038927]高速列车
受电弓平台
[4101116]下沉式
气动力
[8523311]HIGH-SPEED
[100058332]TRAIN
[100212677]PANTOGRAPH
Platform
Sinking-Type
Aerodynamic
Force
Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel
期刊论文
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987
Authors:
Liu YF(刘云峰)
;
Wang YP(汪运鹏)
;
Yuan CK(苑朝凯)
;
Luo ZT(罗长童)
;
Jiang ZL(姜宗林)
;
Liu, YF (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2017/08/22
Aerodynamic Force And Moment Measurement
10° Half-angle Cone Model
Jf12
Real-gas Effects
Shock Tunnel
结构振动对大型激波风洞气动力测量的干扰
期刊论文
力学学报, 2016, 卷号: 48, 期号: 1, 页码: 102-110
Authors:
孟宝清
;
韩桂来
;
姜宗林
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Submit date:2016/03/01
Shock Tunnel
Aerodynamic Force Measurement
Vibration Interference
Theoretical Investigation
Wave system fitting: A new method for force measurements in shock tunnels with long test duration
期刊论文
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2015, 卷号: 62-63, 页码: 2841-2848
Authors:
Luo CT(罗长童)
;
Wang YP(汪云鹏)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
;
Luo, CT (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2016/01/07
Aerodynamic Force Measurements
Strain Gauge Balance
Inertia Compensation
Signal Decomposition
Accelerometer-free
Shock Tunnels
The influence of the fairing shape and cross winds on the aerodynamic characteristics of pantograph
会议论文
THE SECOND INTERNATIONAL CONFERENCE ON RAILWAY TECHNOLOGY: RESEARCH, DEVELOPMENT AND MAINTENANCE, Ajaccio, Corsica, France, 8-11 April 2014
Authors:
Guo DL(郭迪龙)
;
Yao Y
;
Yao SB
;
Yang GW(杨国伟)
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View/Download:94/0
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Submit date:2018/11/08
Flow fields
Lift
Pantographs
Wind
Aerodynamic characteristics
Aerodynamic optimization
Detached eddy simulations
Lift force
Unsteady aerodynamic characteristic
Unsteady aerodynamics
Unsteady characteristics
Vibration
Lattice Boltzmann Simulations of a pitch-up and pitch-down maneuver of a span-wise flexible wing in a free stream flow Read More: http://arc.aiaa.org/doi/abs/10.2514/6.2012-300
会议论文
50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Nashville, TN, United states, JAN 09-12, 2012
Authors:
Qi DW
;
He GW(何国威)
;
Liu YM
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Submit date:2013/02/26
Aerospace Engineering
Deformation
Exhibitions
Flexible Wings
Reynolds Number
Rigidity
Vortex Flow
Aerodynamic Forces
Chord-based Reynolds Number
Flexural Rigidities
Free Stream
Free-stream Flow
Lattice Boltzmann
Leading-edge Vortices
Lift Coefficient
Lift Force
Particle Methods
Pitch Rate
Power Efficiency
Reduced Frequency
Three Dimensional Space
Time-periods
Tip Edge
Trailing Edges
Trailing Vortex