国防科学技术大学 航天科学与工程学院,长沙,410073
Published:2017
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张斌, 杨涛, 丰志伟, 张青斌, 葛健全, 霍霖. 非结构弹性体动网格方法应用策略及改进[J]. 航空动力学报, 2017, 32(3): 648-656.
doi: 10.13224/j.cnki.jasp.2017.03.017
张斌, 杨涛, 丰志伟, 张青斌, 葛健全, 霍霖. 非结构弹性体动网格方法应用策略及改进[J]. 航空动力学报, 2017, 32(3): 648-656. DOI: 10.13224/j.cnki.jasp.2017.03.017.
doi: 10.13224/j.cnki.jasp.2017.03.017 DOI:
针对3种代表性的经典弹性体动网格方法,从网格最大变形能力、质量评价指标和空间分布趋势3个方面综合分析了各方法的网格变形特性,重点总结了各方法的适用范围.结合工程实际,研究了特定问题的弹性体动网格应用策略.最后,整合各经典弹性体动网格方法的优势提出了改进方法,并通过NACA 0006翼型的超声速俯仰振荡加以验证.研究结果表明:基于面积的弹性体法适用于加密型网格,而基于距离的弹性体法适用于均匀型网格,该应用策略可为工程问题提供指导.改进方法效果明显,在大变形时相对基于距离的弹性体法的各项网格质量增幅均在10%以上,相对基于面积的弹性体法的最小网格质量增幅几乎达到4倍,并且在数值模拟中具有较高的精度,可显著增强弹性体法的鲁棒性.
Taking the field of application as a focal point
three classical dynamic grid methods based on elasticity analogy were analyzed in many ways
such as deformation capability
deformation quality and spatial distribution. Combined with engineering demand
the application strategy for grid deformation was presented. Finally
a improvement was proposed for integrating advantages of classical dynamic grid methods based on elasticity analogy
and then verified through pitch oscillation of NACA 0006 airfoil in hypersonic condition. Results show that
when faced with densified grids
the area modification can be controlled better
but faced with uniform grids
the distance modification is more suitable
so this application strategy can provide a guidance for engineering. Secondly
the improvement is accurate in simulation
its all grid quality parameters exceed 10% than classical method based on distance
whats more
its minimum grid quality parameter is about four times the classical method based on area. In conclusion
the improvement is effective in strengthening the robustness of classical elasticity analogy.
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