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Knowledge Management System of Institue of Mechanics, CAS
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State Key ... [7]
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姜宗林 [7]
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汪运鹏 [2]
罗长童 [2]
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Indexed By:EI
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Creator:姜宗林
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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:349/101
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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 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
Intelligent Force-Measurement System Use in Shock Tunnel
期刊论文
SENSORS, 2020, 卷号: 20, 期号: 21, 页码: 6179
Authors:
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
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Submit date:2020/12/28
artificial intelligence
BALANCE SYSTEM
deep learning
DESIGN
dynamic calibration
FLOWS
force-measurement system
strain-gauge balance
A multilevel block building algorithm for fast modeling generalized separable systems
期刊论文
EXPERT SYSTEMS WITH APPLICATIONS, 2018, 卷号: 109, 页码: 25-34
Authors:
Chen C(陈辰)
;
Luo ZT(罗长童)
;
Jiang ZL(姜宗林)
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Submit date:2018/10/30
Symbolic Regression
Genetic Programming
Generalized Separability
Multilevel Block Building
Performance of Copper Calorimeter for Heat Transfer Measurement in High Enthalpy Shock Tunnel
期刊论文
JOURNAL OF THERMAL SCIENCE, 2018, 卷号: 27, 期号: 4, 页码: 373-381
Authors:
Wang Q(汪球)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Jiang ZL(姜宗林)
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Submit date:2018/10/30
copper calorimeter
high enthalpy shock tunnel
heat transfer
hypersonic
Adaptive space transformation: An invariant based method for predicting aerodynamic coefficients of hypersonic vehicles
期刊论文
Engineering Applications of Artificial Intelligence, 2015, 卷号: 46, 页码: 93-103
Authors:
Luo CT(罗长童)
;
Hu ZM(胡宗民)
;
Zhang SL
;
Jiang ZL(姜宗林)
;
Luo, CT (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2016/01/07
Aerodynamic Coefficient
Data Correlation
Scaling Parameter
Genetic Programming
Invariant
Concept of non-ablative thermal protection system for hypersonic vehicles
期刊论文
AIAA Journal, 2013, 卷号: 51, 期号: 3, 页码: 584-590
Authors:
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:1422/511
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Submit date:2013/04/07
Flow Fields
Flow Visualization
Hypersonic Aerodynamics
Hypersonic Vehicles
Mach Number
Shock Waves
Thermal Insulating Materials
Engineering Applications
Experimental Datum
Hypersonic Wind Tunnels
Numerical Results
Stagnation Points
Thermal Protection
Thermal Protection System
Working Pressures