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天宫飞行器低轨控空气动力建模与计算研究进展
  • 所属机构名称：北京航空航天大学
  • 会议名称：第二届全国航天飞行动力学技术研讨会
  • 时间：2013.10.30
  • 成果类型：会议
  • 相关项目：适于千万亿次计算机多相空间数值模拟高性能可扩展并行算法研究
作者： 李志辉|李志辉|
同会议论文项目
适于千万亿次计算机多相空间数值模拟高性能可扩展并行算法研究
期刊论文 44 会议论文 82 获奖 28
同项目会议论文
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求解 Boltzmann 模型方程的高性能并行计算方法研究
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求解热力学非平衡Boltzmann模型方程统一算法与再入气动问题模拟研究
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天宫飞行器低轨控空气动力建模与计算研究进展
Gas-Kinetic Unified Modeling and Massive Parallel Computation of Reentry flows on Complex Bodies
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Gas-Kinetic High-Order Numerical method Solving Boltzmann Model Equation
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Gas-Kinetic High-Order Numerical Method Covering Various Flow Regimes Solving Boltzmann Model Equati
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Gas-Kinetic High-Order Numerical method Solving Boltzmann Model Equation
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求解 Boltzmann 模型方程的高性能并行计算方法研究
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Gas-Kinetic Unified Algorithm for Complex Multi-scale Fluids Covering Various Flow Regimes Solving T
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求解Boltzmann模型方程的高性能并行计算方法研究
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求解热力学非平衡Boltzmann模型方程统一算法与再入气动问题模拟研究
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求解Boltzmann模型方程跨流域空气动力气体动理论统一算法研究
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求解Boltzmann模型方程统一算法与跨流域多尺度绕流高性能计算研究
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