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计算流体力学验证与确认研究进展

陈江涛,肖维,赵炜,张培红,杨福军,金韬,郭勇颜,吴晓军,陈坚强,王瑞利,李立

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陈江涛, 肖维, 赵炜, 张培红, 杨福军, 金韬, 郭勇颜, 吴晓军, 陈坚强, 王瑞利, 李立. 计算流体力学验证与确认研究进展. 力学进展, 2023, 53(3): 626-660 doi: 10.6052/1000-0992-23-012
引用本文: 陈江涛, 肖维, 赵炜, 张培红, 杨福军, 金韬, 郭勇颜, 吴晓军, 陈坚强, 王瑞利, 李立. 计算流体力学验证与确认研究进展. 力学进展, 2023, 53(3): 626-660doi:10.6052/1000-0992-23-012
Chen J T, Xiao W, Zhao W, Zhang P H, Yang F J, Jin T, Guo Y Y, Wu X J, Chen J Q, Wang R L, Li L. Advances in verification and validation in computational fluid dynamics. Advances in Mechanics, 2023, 53(3): 626-660 doi: 10.6052/1000-0992-23-012
Citation: Chen J T, Xiao W, Zhao W, Zhang P H, Yang F J, Jin T, Guo Y Y, Wu X J, Chen J Q, Wang R L, Li L. Advances in verification and validation in computational fluid dynamics.AdvancesinMechanics, 2023, 53(3): 626-660doi:10.6052/1000-0992-23-012

计算流体力学验证与确认研究进展

doi:10.6052/1000-0992-23-012
基金项目:本文工作得到国家数值风洞工程和国家自然科学基金委员会−中国工程物理研究院NSAF联合基金U2230208资助.
详细信息
    作者简介:

    陈江涛, 中国空气动力研究与发展中心副研究员, 主要从事CFD验证与确认及不确定度量化工作. 主持和参与国家数值风洞(NNW)工程验证与确认理论方法专题、共用技术项目、国家自然科学基金重点项目等10余项重大项目. 牵头制定CFD验证与确认标准, 填补国内领域空白. 出版验证与确认领域专著1部, 译著3部, 发表相关论文40余篇

    吴晓军, 中国空气动力研究与发展中心研究员, 国家数值风洞(NNW)工程副总设计师, 验证与确认系统总设计师, 计算空气动力学CFD专委会委员. 长期从事飞行器气动布局设计、飞行器气动关键技术攻关和CFD验证与确认等研究. 先后主持完成国家和省部级重大项目56项, 获省部级科技进步二等奖5项, 三等奖2项, 发表学术论文50余篇, 译著3部

    陈坚强, 中国空气动力研究与发展中心研究员, 空天飞行空气动力科学与技术全国重点实验室主任, 长期从事计算流体力学方法研究、高速复杂流动及工业CFD软件研发等领域的研究工作. 担任国家数值风洞(NNW)工程总设计师, 国家重大研发计划重点专项项目首席科学家. 现任中国空气动力学会副理事长, 计算流体力学专委会主任委员, 《Advances in Aerodynamics》创刊主编及多个杂志编委. 主持研发的自主可控NNW套装软件面向全国发布和开源, 应用于120余家航空航天工业部门和研究院所. 获部委级科技进步一等奖2项, 二等奖8项, 三等奖5项, 发表学术论文160余篇, 出版专著1部

    通讯作者:

    huang7766@sina.com

    chenjq@cardc.cn

  • 中图分类号:O355

Advances in verification and validation in computational fluid dynamics

More Information
  • 摘要:计算流体力学 (CFD) 在重大工程领域发挥了日益重要的作用, 可信度是制约其进一步大规模工程应用的关键因素. 国内外普遍认同验证与确认是CFD可信度评价和保证的必经途径. 通过系统的验证与确认, 可以有效识别代码中潜在的编程错误, 保证数值求解的可靠性, 客观评价模型在预期用途内的适用性, 在必要时提高模型的预测能力. 本文围绕着什么是验证与确认, 怎么做验证与确认这两个核心问题, 从基本概念、实施流程、主要方法、标模试验和平台工具等角度介绍了国内外在CFD验证与确认领域的研究进展, 重点对误差估计和不确定度量化方法展开介绍. 文章最后对现阶段验证与确认研究解决实际工程问题的不足进行了评述和总结, 对未来重点研究方向进行了展望.

  • 图 1第三届AIAA高升力预测会议计算结果汇总(Rumsey et al. 2019)

    图 2国家数值风洞工程验证与确认系统架构

    图 3验证与确认的基本过程 (ASME 2019)

    图 4验证与确认流程图

    图 5高超声速巡航导弹确认层级示例 (Oberkampf & Trucano 2000)

    图 6不确定度量化的关键活动 (NASA 2016b)

    图 7面积度量方法示意图 (夏侯唐凡等2022)

    图 8验证与确认感兴趣的物理问题(Hallissy et al. 2014)

    图 9CHN-T1标模高速风洞油流试验结果

    表 1使用GCI估计数值离散误差时pFs的取值 (Roache 1998)

    $ \left| {\dfrac{{\hat p - {p_{\rm{f}}}}}{{{p_{\rm{f}}}}}} \right| $ Fs p
    $ \leqslant 0.1 $ 1.25 $ {p_{\rm{f}}} $
    $ \gt 0.1 $ 3.0 min(max(0.5, $ \hat p $),$ {p_{\rm{f}}} $)
    下载: 导出CSV
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  • 收稿日期:2023-03-16
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