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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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Indexed By:EI
Date Issued:2015
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Study on Flame Stabilization in a Dual-Mode Combustor Using Optical Measurements
期刊论文
JOURNAL OF PROPULSION AND POWER, 2015, 卷号: 31, 期号: 6, 页码: 1524-1531
Authors:
Yuan YM(袁越明)
;
Zhang TC(张泰昌)
;
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, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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View/Download:517/140
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Submit date:2016/03/21
Lift enhancement by bats' dynamically changing wingspan
期刊论文
Journal of Royal Society Inerface, 2015, 卷号: 12, 页码: 20150821
Authors:
Wang SZ(王士召)
;
Zhang X(张星)
;
He GW(何国威)
;
Liu TS
;
He GW(何国威)
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View/Download:458/92
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Submit date:2016/01/07
Bat Flight
Flapping Flight
Dynamically Changing Wingspan
Unsteady Aerodynamics
An airplane jig shape design method based on high fidelity aeroelastic simulation
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 47, 页码: 314-323
Authors:
Yang W
;
Wang QF
;
Zhou L
;
Zheng GN(郑冠男)
;
Liu W
;
Yang, W (reprint author), Commercial Aircraft Corp China Ltd, Beijing Aeronaut Sci & Technol Res Inst, Beijing, Peoples R China.
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Submit date:2016/03/21
Aeroelasticity
Cfd
Csd
Jig Shape
Structural Mesh
An effective CFD approach for marine-vehicle maneuvering simulation based on hybrid reference frames method
期刊论文
Ocean Engineering, 2015, 卷号: 109, 页码: 83–92
Authors:
Wu XC(吴小翠)
;
Wang YW(王一伟)
;
Huang CG(黄晨光)
;
Hu ZQ
;
Yi RW
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Submit date:2016/01/07
Maneuvering Characteristics
Hybrid Reference Frames Method
Rotating Arm Test
Suboff Model
A novel method of evaluating the lift force on the bluff body based on Noca's flux equation
期刊论文
CHINESE PHYSICS B, 2015, 卷号: 24, 期号: 8, 页码: 84701
Authors:
Sui XK(隋相坤)
;
Jiang N(姜楠)
;
Sui, XK (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
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View/Download:255/94
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Submit date:2016/01/08
Flux Equation
Lift Force
Experimental Error
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
Development of the detonation-driven expansion tube for orbital speed experiments
期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 4, 页码: 695-700
Authors:
Jiang ZL(姜宗林)
;
Wu B(吴波)
;
Gao YL
;
Zhao W(赵伟)
;
Hu ZM(胡宗民)
;
Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:649/157
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Submit date:2015/04/28
Detonation Driver
Shock-expansion Tube
High-enthalpy Flow
Test Flow
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Yao W(姚卫)
;
Wang J(王晶)
;
Lu Y(陆阳)
;
Li XP(李晓鹏)
;
Fan XJ(范学军)
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Submit date:2016/07/01
Adiabatic Flame Temperature
Combustion
Directed Graphs
Flow Separation
Heat Flux
Kerosene
Large Eddy Simulation
Musculoskeletal System
Real Time Systems
Sensitivity Analysis
Spacecraft
Transients
Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel
会议论文
22nd AIAA Computational Fluid Dynamics Conference, 2015, Dallas, TX, United states, June 22, 2015 - June 26, 2015
Authors:
Wang YP(汪运鹏)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
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View/Download:252/48
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Submit date:2017/05/05
Inviscid Flows
Numerical Investigations
Outlet Diameters
Reflected Shock Waves
Simulated Results
Starting Process
Transmitted Shock
Unsteady Nozzle Flow
The Lift Problem in Flapping Forward Flight at Low Reynolds Numbers
会议论文
53rd AIAA Aerospace Sciences Meeting, Kissimmee, Florida, USA, Jan 1-5,2015
Authors:
Liu TS
;
Wang SZ(王士召)
;
Zhang X(张星)
;
He GW(何国威)
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View/Download:313/87
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Submit date:2016/01/07