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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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Date Issued:2015
Language:英语
Community:高温气体动力学国家重点实验室
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Improvement of weighted compact scheme with multi-step strategy for supersonic compressible flow
期刊论文
COMPUTERS & FLUIDS, 2015, 卷号: 115, 页码: 2841-2849
Authors:
Peng J(彭峻)
;
Shen YQ(申义庆)
;
Shen, YQ (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:403/143
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Submit date:2016/01/08
Numerical Method
Supersonic Compressible Flow
Weighted Compact Scheme
Multi-step Strategy
Development and Preliminary Validation of A Thermal Analysis Method for Hydrocarbon Regenerative-cooled Supersonic Combustor
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015
Authors:
Lu Y(陆阳)
;
Wang XZ(王新竹)
;
Li L(李龙)
;
Cheng D(程迪)
;
Yuan T(袁涛)
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(445Kb)
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Submit date:2016/01/08
Hydrocarbons
Combustors
Cooling
Heat Transfer
Near continuum flows over a sphere
期刊论文
COMPUTERS & FLUIDS, 2015, 卷号: 111, 页码: 62-68
Authors:
Cai CP
;
Sun QH(孙泉华)
;
Cai, CP (reprint author), New Mexico State Univ, Dept Mech & Aerosp Engn, Jett Hall 110,MSC 3450, Las Cruces, NM 88003 USA.
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Submit date:2015/04/28
Flow Computation
Navier-stokes Equations
Slip Flows
Direct Numerical Simulation on Mach Number and Wall Temperature Effects in the Turbulent Flows of Flat-Plate Boundary Layer
期刊论文
COMMUNICATIONS IN COMPUTATIONAL PHYSICS, 2015, 卷号: 17, 期号: 1, 页码: 189-212
Authors:
Liang X
;
Li XL(李新亮)
;
Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2015/06/12
Hypersonic
Directly Numerical Simulation
Compressibility Effects
Turbulent Boundary Layer
Strong Reynolds Analogy
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)
Adobe PDF(1195Kb)
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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
Three-dimensional numerical study of the acoustic properities of a highly underexpanded jet
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Wu K(吴坤)
;
Li XP(李晓鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Adobe PDF(590Kb)
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View/Download:396/96
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Submit date:2017/05/05
Frequency Spectrum Analysis
High Temporal Resolution
Instantaneous Flow
Noise Generation Mechanisms
Theoretical Modeling
Three
Dimensional Numerical Studies
Transport Mechanism
Under
Expanded Jets
Numerical Study of Shock/Boundary Layer Interaction of Chemically Reacting Flow in Shock Tube
期刊论文
Procedia Engineering, 2015, 卷号: 126, 页码: 617-621
Authors:
Chen S(陈松)
;
Sun QH(孙泉华)
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Submit date:2016/08/25
Shock/boundary-layer Interaction
Nonequilibrium Chemical Reactions
Shock Tube Flow
Weno Scheme