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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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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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Submit date:2019/01/09
Angle of attack
Fiber Bragg grating sensor
Flow velocity
Internal pressure
Non-rigid airship
Wind tunnel test
Shock/shock interactions between bodies and wings
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 2, 页码: 255-261
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Teng HH(腾宏辉)
;
Jiang ZL(姜宗林)
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Submit date:2018/10/30
Body And Wing
Flow Field
Hypersonic Flow
Shock/shock Interaction
Wave Configurations
High-speed unsteady flows past two-body configurations
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 1, 页码: 54-64
Authors:
Xue XP
;
Nishiyama Y
;
Nakamura Y
;
Mori K
;
Wang YP(汪运鹏)
;
Wen CY
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Submit date:2018/10/30
Compressible flow
Shock/shock interaction
Two-body configurations
Unsteady flow
Wake/shock interaction
Numerical studies of static aeroelastic effects on grid fin aerodynamic performances
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2017, 卷号: 30, 期号: 4, 页码: 1300-1314
Authors:
Huang CD(黄程德)
;
Liu W(刘文)
;
Yang GW(杨国伟)
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Submit date:2017/11/29
Aeroelasticity
Fluid-structure Interpolation
Grid Fin
Mesh Deformation
Radial Basis Function
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
A quasi-one-dimensional model for hypersonic reactive flow along the stagnation streamline
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2016, 卷号: 29, 期号: 6, 页码: 1517-1526
Authors:
Chen Song
;
Sun QH(孙泉华)
;
Sun, QH (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:2017/04/26
A novel intelligent adaptive control of laser-based ground thermal test
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2016, 卷号: 29, 期号: 4, 页码: 1018-1026
Authors:
Gan ZT
;
Yu G(虞刚)
;
Li SX(李少霞)
;
He XL(何秀丽)
;
Chen R
;
Zheng CY(郑彩云)
;
Ning WJ(宁伟健)
;
Yu, G (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Adv Mfg, Beijing 100190, Peoples R China.
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Submit date:2016/12/08
Adaptive Control
Fuzzy Logic
Ground Thermal Test
Laser Heating
Thermal Control
Radical recombination in a hydrocarbon-fueled scramjet nozzle
期刊论文
Chinese Journal of Aeronautics, 2014, 卷号: 27, 期号: 6, 页码: 1413-1420
Authors:
Zhang XY(张晓源)
;
Qin LZ
;
Chen H(陈宏)
;
He XZ
;
Liu Y
;
Qin, LZ (reprint author), Beihang Univ, Sch Astronaut, Beijing 100191, Peoples R China.
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Submit date:2015/03/11
Chemical Reactions
Nozzles
Performance Calculation
Radical
Recombination
Improvement of Baldwin-Lomax turbulence model for supersonic complex flows
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 期号: 3, 页码: 529–534
Authors:
Zhao R(赵瑞)
;
Yan C(阎超)
;
Yu J(于剑)
;
Li XL(李新亮)
;
Yan, C (reprint author), Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China.
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Submit date:2013/09/21
Baldwin-lomax Model
Boundary Layers
Computational Aerodynamics
Entropy
Supersonic Flows
Turbulence Models
Research on modeling of heat source for electron beam welding fusion-solidification zone
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 期号: 1, 页码: 217-223
Authors:
Wang YJ
;
Fu PF
;
Guan YJ(关永军)
;
Lu ZJ
;
Wei YT
;
Wang, YJ (reprint author), Beihang Univ, Sch Mech Engn & Automat, Beijing 100191, Peoples R China.
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Submit date:2013/04/07
Electron Beam Welding (Ebw)
Fusion-solidification Zone
Heat Source Model
Temperature Fields
Weld Shape