| 机体/动力装置一体化分析中的动力影响效应数值模拟 |
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| 引用本文： | 谭兆光,陈迎春,李杰,张淼.机体/动力装置一体化分析中的动力影响效应数值模拟[J].航空动力学报,2009,24(8):1766-1772. |
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| 作者姓名： | 谭兆光 陈迎春 李杰 张淼 |
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| 作者单位： | 西北工业大学航空学院;中国商用飞机公司上海飞机设计研究所; |
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| 基金项目： | 国家自然科学基金(10772148) |
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| 摘 要： | 采用合适的进、排气边界条件,对带动力的单独涡扇发动机模型和带动力的DLR-F6翼身架舱复杂组合体(WBPN)模型的流场进行了数值模拟和分析.运用Roe三阶迎风偏置通量差分裂方法和隐式近似因子分解方法求解雷诺平均Navier-Stokes方程,基于点搭接多块网格技术生成高质量计算网格,通过多重网格技术来加速收敛.着重对动力发动机进、排气边界条件的给定进行了推导,以准确地模拟发动机动力效应.计算结果与实验值吻合良好,验证了所采用计算方法、网格分块策略和边界条件处理方法的正确性.
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| 关 键 词： | 动力发动机 边界条件 Navier-Stokes方程 多重网格技术 多块网格 一体化分析 |
| 收稿时间： | 7/28/2008 9:12:27 AM |
| 修稿时间： | 2008/12/12 0:00:00 |
Numerical simulation method for the powered effects in airframe/propulsion integration analysis |
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| TAN Zhao-guang,CHEN Ying-chun,LI Jie and ZH ANG Miao.Numerical simulation method for the powered effects in airframe/propulsion integration analysis[J].Journal of Aerospace Power,2009,24(8):1766-1772. |
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| Authors: | TAN Zhao-guang CHEN Ying-chun LI Jie and ZH ANG Miao |
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| Institution: | 1.College of Aeronautics;Northwestern Polytechnical University;Xi'an 710072;China;2.Shanghai Aircraft Design and Research Institute;Commercial Aircraft Corporation of China;Shanghai 200232;China |
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| Abstract: | The flow-fields around powered isolated turbofan engine model and powered DLR-F6 wing/body/pylon/nacelle(WBPN) model were numerically simulated and analyzed by the appropriate fan inlet face and jet-exit boundary conditions.Three-dimensional time-dependent compressible Reynolds-averaged Navier-Stokes equations were solved with third-order upwind-biased flux-difference splitting method and approximate factorization method.The point-to-point patched multi-block technology was used to generate high quality gri... |
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| Keywords: | powered engine boundary conditions Navier-Stokes equations multi-grid technique multi-block grid integration analysis |
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