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Gaseous Detonation Physics and Its Universal Framework Theory 专著
Beijing:Springer Nature, 2022
作者:  Jiang ZL(姜宗林);  Teng, Honghui
Adobe PDF(13641Kb)  |  收藏  |  浏览/下载：105/2  |  提交时间：2023/03/23
On the design of potential turbine positions for physics-informed optimization of wind farm layout 期刊论文
RENEWABLE ENERGY, 2021, 卷号: 164, 页码: 1108-1120
作者:  Wu, Chutian;  Yang, Xiaolei;  Zhu, Yaxin
Adobe PDF(4543Kb)  |  收藏  |  浏览/下载：258/52  |  提交时间：2021/01/12
Wind farm layout optimization  Physics-informed  Potential turbine positions  Jensen wake model  Genetic algorithm  
A new front tracking method using particles with extended location information 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2019, 卷号: 378, 页码: 497-547
作者:  Fan P(范平)
浏览  |  Adobe PDF(7065Kb)  |  收藏  |  浏览/下载：265/81  |  提交时间：2019/04/11
Moving interface  Front tracking  Numerical scheme  Extended location information  
Numerical Analysis of Transient Pressure Behaviors with Shale Gas MFHWs Interference 期刊论文
ENERGIES, 2019, 卷号: 12, 期号: 2, 页码: 21
作者:  Gao DP(高大鹏);  Liu YW(刘曰武);  Wang DG;  Han GF(韩国锋)
浏览  |  Adobe PDF(7266Kb)  |  收藏  |  浏览/下载：253/41  |  提交时间：2019/04/11
shale gas  multi-stage fracturing horizontal wells  well interference  transient pressure  numerical analysis  
Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
作者:  Yao W(姚卫);  Li B(李波)
Adobe PDF(1665Kb)  |  收藏  |  浏览/下载：143/43  |  提交时间：2020/11/20
Dynamic zone flamelet model  GH2/GO2  Large Eddy Simulation (LES)  Rocket combustor  Turbulence-chemistry interaction  
Bifurcations of vortex-induced vibrations of a fixed membrane wing at Re 1000 期刊论文
NONLINEAR DYNAMICS, 2018, 卷号: 91, 期号: 4, 页码: 2097-2112
作者:  Sun X;  Wang SZ(王士召);  Zhang JZ;  Ye ZH
浏览  |  Adobe PDF(7313Kb)  |  收藏  |  浏览/下载：224/63  |  提交时间：2018/10/30
Membrane wing  Vortex-induced vibration  Numerical simulation  Bifurcation  Fluid-structure interaction  
Uncertain reduced-order modeling for unsteady aerodynamics with interval parameters and its application on robust flutter boundary prediction 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 214-230
作者:  Chen XJ;  Qiu ZP;  Wang XJ;  Li YL;  Wang RX(王睿星)
浏览  |  Adobe PDF(4860Kb)  |  收藏  |  浏览/下载：390/87  |  提交时间：2018/02/08
Uncertain Reduced-order Modeling  Robust Flutter Analysis  Interval Perturbation Method  Uncertain Aeroelastic System  
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
作者:  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.
浏览  |  Adobe PDF(5723Kb)  |  收藏  |  浏览/下载：418/183  |  提交时间：2017/11/16
Underexpanded Jets  Noncircular Jets  Nozzle Geometry  Large Eddy Simulation  
A 3D coupled model of organic matter and inorganic matrix for calculating the permeability of shale 期刊论文
FUEL, 2017, 卷号: 204, 页码: 129-143
作者:  Cao GH(曹高辉);  Lin M(林缅);  Jiang WB(江文滨);  Li HS;  Yi ZX;  Wu CJ;  Lin, M (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(4194Kb)  |  收藏  |  浏览/下载：625/193  |  提交时间：2017/08/15
Multiscale  3d Coupled Model  Mortar  Apparent Permeability  Shale Gas  
Development of zone flamelet model for scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(623Kb)  |  收藏  |  浏览/下载：263/90  |  提交时间：2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft