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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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Flow characteristic of highly underexpanded jets from various nozzle geometries
期刊论文
APPLIED THERMAL ENGINEERING, 2017, 卷号: 125, 页码: 240-253
Authors:
Li XP(李晓鹏)
;
Zhou, Rui
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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View/Download:448/194
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Submit date:2017/11/16
Underexpanded Jets
Noncircular Jets
Nozzle Geometry
Large Eddy Simulation
Particle-Based Modeling of Asymmetric Flexible Fibers in Viscous Flows
期刊论文
COMMUNICATIONS IN COMPUTATIONAL PHYSICS, 2017, 卷号: 22, 期号: 4, 页码: 1015-1027
Authors:
Yang XF(杨秀峰)
;
Liu MB(刘谋斌)
;
Liu, MB (reprint author), Peking Univ, Coll Engn, BIC ESAT, Beijing 100187, Peoples R China.
;
Liu, MB (reprint author), Peking Univ, State Key Lab Turbulence & Complex Syst, Beijing 100871, Peoples R China.
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Submit date:2017/10/27
Fluid-structure Interaction
Asymmetric Flexible Fiber
Drag Force
Smoothed Particle Hydrodynamics (Sph)
Element Bending Group (Ebg)
Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp
会议论文
Meeting of the Institute-of-Non-Newtonian-Fluid-Mechanics (INNFM), Llanwddyn, WALES, 2017
Authors:
Tong FL(童福林)
;
Li XL(李新亮)
;
Duan, Yanhui
;
Yu ZP(于长平)
;
Yu, CP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Submit date:2018/01/16
Concave Surface Curvature
Adverse Pressure-gradient
Large-eddy Simulation
Reynolds-number
Near-wall
Flows
Separation
Vortices
Models
INVESTIGATION OF OBSTACLE EFFECTS ON THE AERODYNAMIC PERFORMANCE OF FLAPPING WINGS
会议论文
ASME Fluids Engineering Division Summer Meeting, Waikoloa, HI, JUL 30-AUG 03, 2017
Authors:
Yin B(银波)
;
Yang GW(杨国伟)
;
Yin, B (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing, Peoples R China.
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Submit date:2018/01/16
Immersed-boundary Method
Micro-air Vehicles
Insect Flight
Vortices
Forces
Flows
Self-propelled swimming of a flexible plunging foil near a solid wall
期刊论文
BIOINSPIRATION & BIOMIMETICS, 2016, 卷号: 11, 期号: 4, 页码: 46005
Authors:
Dai LZ
;
He GW(何国威)
;
Zhang X(张星)
;
Zhang, X (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
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Submit date:2016/07/11
Wall Effect
Self-propulsion
Flapping Foil
Flexibility
Biolocomotion
An experimental study of the effects of pitch-pivot-point location on the propulsion performance of a pitching airfoil
期刊论文
JOURNAL OF FLUIDS AND STRUCTURES, 2016, 卷号: 60, 页码: 130-142
Authors:
Tian W
;
Bodling A
;
Liu H
;
Wu JC
;
He GW(何国威)
;
Hu H
;
Hu, H (reprint author), Iowa State Univ, Dept Aerosp Engn, Ames, IA 50010 USA.
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Submit date:2016/03/21
Micro-air-vehicles (Mavs)
Unsteady Aerodynamics
Pitching Airfoil
Pitch-pivot-point Location
Piv
Unsteady Thin-Airfoil Theory Revisited: Application of a Simple Lift Formula
期刊论文
AIAA Journal, 2015, 卷号: 53, 期号: 6, 页码: 1492-1502
Authors:
Liu TS
;
Wang SZ(王士召)
;
Zhang X(张星)
;
He GW(何国威)
;
Liu, TS (reprint author), Western Michigan Univ, Dept Mech & Aerosp Engn, Kalamazoo, MI 49008 USA.
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Submit date:2016/01/08
Evaluation of Lift Formulas Applied to Low-Reynolds-Number Unsteady Flows
期刊论文
AIAA Journal, 2015, 卷号: 53, 期号: 1, 页码: 161-175
Authors:
Wang SZ(王士召)
;
Zhang X(张星)
;
He GW(何国威)
;
Liu TS
;
He, GW (reprint author), Chinese Acad Sci, State Key Lab Nonlinear Mech, Inst Mech, Beijing 100190, Peoples R China.
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View/Download:394/106
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Submit date:2015/03/17
Smoothed particle hydrodynamics and element bending group modeling of flexible fibers interacting with viscous fluids
期刊论文
PHYSICAL REVIEW E, 2014, 卷号: 90, 期号: 6, 页码: 63011
Authors:
Yang XF(杨秀峰)
;
Liu MB(刘谋斌)
;
Peng SL(彭世镠)
;
Yang, XF (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2015/01/23
Lift enhancement by dynamically changing wingspan in forward flapping flight
期刊论文
PHYSICS OF FLUIDS, 2014, 卷号: 26, 期号: 6, 页码: 61903
Authors:
Wang SZ(王士召)
;
Zhang X(张星)
;
He GW(何国威)
;
He, GW (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
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View/Download:804/186
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Submit date:2014/11/03
Immersed Boundary Method
Leading-edge Vortices
Insect Flight
Aerodynamic Performance
Unsteady Aerodynamics
Wake Structure
Free Vortex
Bat Flight
Kinematics
Flow