Effect of Porosity and Injection Ratio on the Performance of Transpiration Cooling through Gyroids

IF 1.3 Q2 ENGINEERING, AEROSPACE
Benjamin J. Brimacombe, James A. Scobie, Joseph M. Flynn, C. Sangan, Oliver J Pountney
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引用次数: 0

Abstract

This paper presents experimental measurements of adiabatic effectiveness for three transpiration cooling porosities (ϕ= 0.3, 0.4, and 0.5) constructed from gyroid lattice structures. To the authors’ knowledge, this is the first use of a Triply Periodic Minimal Surface (TPMS) function to produce transpiration test coupons of varying porosity. Polymer gyroid lattice structures were successfully printed using Stereolithography (SLA) down to ϕ= 0.3 for a print resolution of 25 microns and unit cell size of 2 mm. Cooling performance was measured in a small-scale wind tunnel. High-resolution Infrared Thermography was used to determine wall temperatures downstream of the porous section. When tested at both common blowing ratios (M = 0.029, 0.048, and 0.062) and common injection ratios (F = 0.010, 0.017, and 0.022) the cooling performance was found to be dependent on porosity for constant M but not for constant F. Having determined F as the more important parameter for comparison, results are presented alongside transpiration and effusion data from literature.
孔隙率和喷射比对通过陀螺仪进行蒸气冷却的性能的影响
本文提出了三种蒸腾冷却孔隙(φ = 0.3, 0.4和0.5)的绝热有效性的实验测量由陀螺晶格结构构成。据作者所知,这是第一次使用三周期最小表面(TPMS)函数来产生不同孔隙度的蒸腾试验片。利用立体光刻技术(SLA)成功打印了聚合物陀螺晶格结构,其ϕ= 0.3,打印分辨率为25微米,单元尺寸为2毫米。在一个小型风洞中测量了冷却性能。采用高分辨率红外热像仪测定多孔截面下游的壁温。在常规吹气比(M = 0.029、0.048和0.062)和常规喷射比(F = 0.010、0.017和0.022)下进行测试时,发现恒定M时的冷却性能取决于孔隙度,而恒定F时则无关。确定F为更重要的比较参数后,结果与文献中的蒸腾和渗出数据一起呈现。
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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来源期刊
CiteScore
2.30
自引率
21.40%
发文量
29
审稿时长
11 weeks
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