Numerical Study on Convective Heat Transfer Performance in Helix Lattice Sandwich Panel

Shulei Li, Shibo Zhang, G. Xie, Hongbin Yan
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Abstract

Sandwich structures have been widely used as thermal and load-bearing materials in astronautic and aeronautic applications. owing to their advantages of high specific strength and stiffness. Among them, the X-type lattice cored sandwich panel has a superior thermal performance, with a larger pressure drop. In order to solve the disadvantage of higher pressure drop of the X-type lattice, this paper propose a new structure of helix lattice sandwich panel by modifying the structure of the X-type lattice at a similar porosity level. Forced convection of air in the helix lattice sandwich panel was numerically studied based on the validated model in available literature. The flow and heat transfer characteristics between the helix lattice and X-type lattice were compared. Results reveal that the fluid flow pattern of the helix lattice and the X-type lattice have similarities and differences. The similarity is that both of them cause a spiral type of flow and two same type of secondary flow, the difference is that compared with X-type lattice, the smaller blockage of flow area by the ligaments of the helix lattice leads to a large smooth mainstream. Besides, the overall Nusselt number of the helix lattice is slightly lower than that of X-type one with an average value of 6.69% at a certain Reynolds number, the same material thermal conductivity and similar porosity level. Although the flow pattern in the helix lattice is similar to that in X-type lattice, the smooth mainstream in the helix lattice inevitably limited the flow mixing which lead to a lower area-averaged Nusslet number on both the substrates and the ligaments relative to X-type one. However, in terms of pressure drop, the helix lattice is significantly lower than the X-type lattice due to smaller flow area blockage and smooth ligament structure, which is reduced by nearly half. The helix lattice core sandwich panel can maintain a high level heat transfer performance with little loss of pressure drop. For a given pumping power, the helix lattice outperforms X-type lattice by up to 6.65%. Furthermore, as the pumping power increases, the heat transfer performance of the helix lattice will be better than X-type lattice. Therefore, it can be considered that the helix lattice core sandwich panel solves the disadvantage of relatively high pressure drop in the X-type lattice, greatly reduced the pressure drop and the required pumping power with less heat transfer performance loss. The helix lattice core sandwich panel has a superior comprehensive heat transfer performance than X-type one.
螺旋晶格夹层板对流换热性能的数值研究
夹层结构作为热材料和承载材料在航空航天领域得到了广泛的应用。由于其具有高比强度和刚度的优点。其中,x型点阵芯夹芯板的热性能优越,压降较大。为了解决x型晶格压降较高的缺点,本文在相似孔隙度的条件下,通过对x型晶格结构进行修改,提出了一种螺旋晶格夹层板的新结构。在现有文献验证模型的基础上,对螺旋晶格夹层板内空气强制对流进行了数值研究。比较了螺旋晶格和x型晶格之间的流动和传热特性。结果表明,螺旋晶格与x型晶格的流体流动形态既有相似之处,也有不同之处。相似之处在于两者都产生了螺旋型流动和两种相同类型的二次流,不同之处在于与x型晶格相比,螺旋晶格的韧带对流动面积的阻塞越小,就会产生较大的光滑主流。在一定雷诺数、材料导热系数相同、孔隙率相近的条件下,螺旋晶格的整体努塞尔数略低于x型晶格,平均值为6.69%。虽然螺旋晶格中的流动模式与x型晶格相似,但螺旋晶格中光滑的主流不可避免地限制了流动的混合,从而导致衬底和韧带上的面积平均努斯莱特数相对于x型晶格都要低。但在压降方面,螺旋晶格由于流区堵塞较小,韧带结构光滑,压降明显低于x型晶格,降低了近一半。螺旋晶格芯夹芯板可以保持高水平的传热性能,而压降损失很小。对于给定的泵送功率,螺旋晶格比x型晶格性能高6.65%。此外,随着泵送功率的增加,螺旋晶格的传热性能将优于x型晶格。因此,可以认为螺旋晶格芯夹芯板解决了x型晶格压降较高的缺点,大大降低了压降和所需的泵送功率,传热性能损失较小。螺旋格芯夹层板综合传热性能优于x型夹层板。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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