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[会议论文] 作者:Zhang Hanxin,Xu Hongguo, 来源:第八届全国交通运输领域青年学术会议 年份:2009
In this paper,the quicky development of bicycle is taken as example to solve the issues and amends in the traffic accident.From three aspects of the vehicle,the un-motorizing vehicle and the human whi...
[期刊论文] 作者:ZHANG HanXin, ZHANG Zhao, YUAN, 来源:中国科学:技术科学英文版 年份:2007
Analytical methods of nonlinear dynamics and numerical simulations for the cou-pling equations of Navier-Stokes and flight mechanics are used to study the dynam...
[期刊论文] 作者:Shen Qing Zhang Hanxin Yuan Xi, 来源:空气动力学学报 年份:2000
本文通过有限差分计算求解了NS方程,对超声速二维平板边界层的非线性稳定性问题进行了模拟.流场的来流马赫数为4.5.平板从尖前缘开始,流场在前缘处产生一道前缘激波.数值计算...
[期刊论文] 作者:LI Zhihui,ZHANG Hanxin,FU Song, 来源:中国科学G辑(英文版) 年份:2005
The gas-kinetic unified algorithm using Boltzmann model equation have been extended and developed to solve the micro-scale gas flows in Poiseuille-like micro-ch...
[期刊论文] 作者:ZHANG HanXin,ZHANG Zhao,YUAN X, 来源:中国科学E辑 年份:2004
Analytical methods of nonlinear dynamics and numerical simulations for the coupling equations of Navier-Stokes and flight mechanics are used to study the dynami...
[期刊论文] 作者:ZHANG HanXin,ZHANG Zhao,YUAN X, 来源:黑龙江科技学院学报 年份:2007
为探究吕家坨井田地质构造格局,根据钻孔勘探资料,采用分形理论和趋势面分析方法,研究了井田7...
[期刊论文] 作者:Li Chen,Guo Qilong,Li Qin,Zhang Hanxin,, 来源:Transactions of Nanjing University of Aeronautics and Astron 年份:2017
A novel third-order optimized symmetric weighted essentially non-oscillatory(WENO-OS3)scheme is used to simulate the hypersonic shock wave/boundary layer intera...
[会议论文] 作者:Liu Xuliang,Zhang Shuhai,Zhang Hanxin,Chi-Wang Shu, 来源:2013中国力学大会 年份:2013
In this talk,we will report a new class of central compact schemes and its application to the interaction of the two isentropic vortices.The scheme is proposed based on the cell-centered compact schem...
[期刊论文] 作者:LI Chen1,2, GUO Qilong1,2, LI Qin1,2*, ZHANG Hanxin1,2, 来源:Transactions of Nanjing University of Aeronautics & Astronau 年份:
In this paper, a new third-order optimized symmetric weighted essentially non-oscillatory (WENO-OS3) scheme is used to simulate the hypersonic shock wave/bounda...
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