MOVING

作品数:977被引量:1459H指数:15
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相关作者:万德成何湘君杨元喜张勤张双成更多>>
相关机构:清华大学天津工程机械研究院华中科技大学西南交通大学更多>>
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A three-dimensional inverse method based on moving no-slip boundary for profiled end wall design
《Chinese Journal of Aeronautics》2024年第10期221-233,共13页Hanwen GUO Donghai JIN Jiancheng ZHANG Xingmin GUI 
Supported by the National Natural Science Foundation of China(No.52376021).
How to utilize existing flow control mechanisms to make profiled end wall design more flexible,efficient,and physical is a meaningful challenge.This study presents a three-dimensional inverse method for profiled end w...
关键词:COMPRESSOR Flow control Corner separation Profiled end wall Inverse method 
Stage separation of recoverable liquid launch vehicle by using moving pulsating ball analogue for propellant sloshing
《Chinese Journal of Aeronautics》2024年第2期360-370,共11页Yu LU Baozeng YUE Bailong HAO Bole MA Feng LIU Yuanyuan CHANG 
supported by the National Natural Science Foundation of China(Nos.12132002,12202044)。
In the process of stage separation of recoverable liquid launch vehicles,because of the large amount of residual fuel in the storage tanks,the influence of liquid sloshing on separation safety must be considered.Consi...
关键词:Moving Pulsating Ball Model(MPBM) Dynamics of stage separation Large amplitude sloshing Recoverable liquid launch vehicle Flight dynamics 
A partition of unity level set method with moving knot CS-RBFs for optimizing variable stiffness composites被引量:2
《Chinese Journal of Aeronautics》2023年第4期565-572,共8页Gen LI Ye TIAN Kang YANG Tielin SHI Qi XIA 
supported by the National Natural Science Foundation of China(No.51975227).
A partition of unity level set method with moving knot Compactly Supported Radial Basis Functions(CS-RBFs)is proposed for optimizing variable stiffness composite structures.The iso-contours of a level set function are...
关键词:Composite structures Moving knots Partition of unity Radial basis functions Structural optimization 
Ground-based investigations on phase-moving phenomenon with space sublimation cooling for lunar exploration missions被引量:3
《Chinese Journal of Aeronautics》2022年第8期65-74,共10页Enhui LI Yunze LI Jixiang WANG Man YUAN Jingyan XIE Yuehang SUN Lizhu YANG Xianwen NING 
primarily funded by the cooperative project offered by Beijing Key Laboratory of Space Thermal Control Technology;funded by China Postdoctoral Science Foundation(No.2020 M671618)。
The lunar surface is a typical vacuum environment,and its harsh heat rejection conditions bring great challenges to the thermal control technology of the exploration mission.In addition to the radiator,the sublimator ...
关键词:Lunar vacuum environment Phase-change flow Space sublimation cooling Unsteady phase-moving phenomenon Visualized ground-based experimental approaches 
Reflection of a moving shock wave over an oblique shock wave
《Chinese Journal of Aeronautics》2021年第5期399-403,共5页Miaomiao WANG Ziniu WU 
supported partly by the National Key Project(No.GJXM92579);the National Science and Technology Major Project(No.2017-II-003-0015)。
The reflection of a moving shock wave over a wedge immersed in a still gas and the reflection of a wed ge induced steady shock wave over symmetrical and asymmetrical reflecting surfaces have received intensive conside...
关键词:Shock reflection Triple point Unsteady shock wave 
Ferrofluid moving thin films for active flow control被引量:3
《Chinese Journal of Aeronautics》2021年第5期115-119,共5页Francisco J.ARIAS 
supported by the Spanish Ministry of Economy and Competitiveness under Fellowship Grant Ramon y Cajal(No.RYC-2013-13459)。
Ferrofluid moving thin films and their possible significance with regard to active flow control for lift and attack angle enhancement are discussed.In this strategy,a very thin film of ferrofluid is strongly attached ...
关键词:Active flow control Boundary layer separation FERROFLUID 
High precision attitude dynamic tracking control of a moving space target被引量:7
《Chinese Journal of Aeronautics》2019年第10期2324-2336,共13页Yunhua WU Mohong ZHENG Wei HE Feng WANG Zhiming CHEN Bing HUA 
the support provided by the National Natural Science Foundation of China(No.61973153);the National Key Research and Development Plan of China(No.2016YFB0500901);the Open Fund of the National Defense Key Discipline Laboratory of Micro-Spacecraft Technology of China(No.HIT.KLOF.MST.201705)
On-orbit spacecraft face many threats,such as collisions with debris or other spacecraft.Therefore,perception of the surrounding space environment is vitally important for on-orbit spacecraft.Spacecraft require a dyna...
关键词:Space MOVING target ATTITUDE DYNAMIC tracking BACKSTEPPING controller Improved virtual control input Hybrid ACTUATOR 
An improved analytical model of cutting temperature in orthogonal cutting of Ti6Al4V被引量:10
《Chinese Journal of Aeronautics》2019年第3期759-769,共11页Chenwei SHAN Xu ZHANG Bin SHEN Dinghua ZHANG 
co-supported by National Science and Technology Major Project of China (No. 2015ZX04004001);National Natural Science Foundation of China (No. 51875473);Natural Science Foundation of Shaanxi province of China (No. 2017JM5027);Fundamental Research Funds for the Central Universities of China (No. 3102017gx06007)
Cutting heat has significant effects on the machined surface integrity of titanium alloys in the aerospace field. Many unwanted problems such as surface burning, work hardening, and tool wear can be induced by high cu...
关键词:CUTTING temperature MOVING heat source method ORTHOGONAL CUTTING RELIEF angle TITANIUM alloy 
Fault mode probability factor based fault-tolerant control for dissimilar redundant actuation system被引量:1
《Chinese Journal of Aeronautics》2018年第5期965-975,共11页Jun WANG Shaoping WANG Xingjian WANG Mileta M.TOMOVIC Cun SHI 
co-supported by the National Natural Science Foundation of China(Nos.51620105010,51675019 and 51575019);the National Basic Research Program of China(No.2014CB046402);the Fundamental Research Funds for the Central Universities of China(YWF-17-BJ-Y-105);the "111" Project of China
This paper presents a Fault Mode Probability Factor(FMPF) based Fault-Tolerant Control(FTC) strategy for multiple faults of Dissimilar Redundant Actuation System(DRAS)composed of Hydraulic Actuator(HA) and Ele...
关键词:Dissimilar redundant actuation system Fault mode probability factor Fault-tolerant control Linear quadratic regulator Monte Carlo simulation Moving window 
Robust Navier-Stokes method for predicting unsteady flowfield and aerodynamic characteristics of helicopter rotor被引量:24
《Chinese Journal of Aeronautics》2018年第2期214-224,共11页Qijun ZHAO Guoqing ZHAO Bo WANG Qing WANG Yongjie SHI Guohua XU 
co-supported by the National Natural Science Foundation of China (Nos. 11272150, 10872094 and 10602024)
A robust unsteady rotor flowfield solver CLORNS code is established to predict the complex unsteady aerodynamic characteristics of rotor flowfield. In order to handle the difficult problem about grid generation around...
关键词:Aerodynamic characteristicsHelicopter rotor Moving-embedded grid Navier-Stokes equations Upwind schemes 
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