跨流域高超声速绕流环境Boltzmann模型方程统一算法研究∗OA北大核心CSCDCSTPCD
Gas-kinetic unified algorithm for hyp ersonic aerothermo dynamics covering various flow regimes solving Boltzmann mo del equation
How to solve hypersonic aerothermodynamics and complex flow mechanism covering various flow regimes from high rarefied free-molecular flow of outer-layer space to continuum flow of near-ground is one of the frontier basic problems in the field of fluid physics. In this work, the unified Boltzmann model equation based on the molecular velocity distribution function is presented for describing complex hypersonic flow transport phenomena covering all flow regim…查看全部>>
李志辉;彭傲平;方方;李四新;张顺玉
中国空气动力研究与发展中心超高速空气动力研究所，绵阳 621000 中国空气动力研究与发展中心，空气动力学国家重点实验室，绵阳 621000中国空气动力研究与发展中心超高速空气动力研究所，绵阳 621000中国空间技术研究院，载人航天总体部，北京 100094中国空气动力研究与发展中心超高速空气动力研究所，绵阳 621000
Boltzmann模型方程离散速度坐标法跨流域统一算法高超声速流动
Boltzmann model equationdiscrete velocity ordinate methodgas-kinetic unified algorithm covering various flow regimeshypersonic flows
《物理学报》 2015 (22)
近空间飞行器跨流域复杂非平衡绕流问题的模拟研究
1-17,17
国家重点基础研究发展计划(批准号:2014CB744100)、国家自然科学基金(批准号:11325212,91016027)和国防基础科研基金(批准号:51313030104)资助的课题.* Project supported by the National Basic Research Program of China (Grant No.2014CB744100), the National Natural Science Foundation of China (Grant Nos.11325212,91016027), and the National Defense Basic Scientific Research Program of China (Grant No.51313030104)
评论