火焰筒多斜邻接孔冷却特性数值模拟分析OA
Numerical Simulation of Cooling Characteristics for Multi-angled Adjacent Holes in Flame Tubes
为提升燃烧室火焰筒冷却性能,优化多斜邻接孔冷却结构,在冷热流温度比为0.43、冷热流质量流率分别为85 m3/h和580 m3/h、开孔率一致的条件下,采用Fluent软件,将火焰筒壁面平板化进行数值模拟,分析对比热侧壁面温度分布、流向及展向的沿程综合冷效(φ)、流量系数(Cd)、流向及展向的表面传热系数比(h/h0),研究不同大孔孔径(D)与大孔展向中心间距(Y1)对火焰筒壁面冷却特性的影响.结果表明:D与Y1较小时能在热侧壁面快速形成连续且均匀的低温区,D从0.8 mm增至1.5 mm后流向φ峰值下降17.5%,展向φ均值降低14.5%;与D=0.8 mm模型相比,D=1.4 mm、1.5 mm模型的Cd分别提高122.2%、188.8%;较小的D与Y1热侧壁面以低强度剪切涡为主,湍动能集中于近壁区域(Y<3 mm),最大湍动能约为95 m2/s2,D与Y1增大将导致气膜剪切层分离加剧,形成较大尺度肾形涡;所有模型在0<X<20 mm区间的流向h/h0为3.1~5.2,在X=30~60 mm区间时流向h/h0数值稳定在1.5~2.1,反映气膜层对热流的有效隔离,D=1.3 mm模型的展向边缘区域(Z=25~30 mm)的h/h0峰值可达2.4,相较于D=0.8 mm模型的展向h/h.峰值升高约14.2%.
To enhance the cooling performance of the combustion chamber flame tube and optimize the cooling structure of multi-angled adjacent holes,numerical simulations were conducted using Fluent soft-ware under the conditions of coolant-to-mainstream temperature ratio of 0.43,mass flow rates of 85 m3/h and 580 m3/h for the coolant and mainstream respectively,while maintaining consistent porosity.The flame tube wall was simplified as a flat plate for simulation.The effects of different main-hole diame-ters(D)and the spanwise center-to-center spacing between main holes(Y1)on the cooling characteris-tics of the flame tube wall were investigated by analyzing and comparing the temperature distribution on the hot-side wall,the streamwise and spanwise distributions of overall cooling effectiveness(φ),the dis-charge coefficient(Cd),and the streamwise and spanwise surface heat transfer coefficient ratio(h/h0).The results show that smaller D and Y1 values can rapidly form a continuous and uniform low-tempera-ture zone on the hot-side wall.When D increases from 0.8 mm to 1.5 mm,the peak streamwise φ decrea-ses by 17.5%,and the spanwise average φ reduces by 14.5%.Compared to the model with D=0.8 mm,the Cd of models with D=1.4 mm and 1.5 mm increases by 122.2%and 188.8%,respectively.For smal-ler D and Y1,the hot-side wall is dominated by low-intensity shear vortices,with turbulent kinetic ener-gy concentrated in the near-wall region(Y<3 mm),reaching a maximum value of approximately 95 m2/s2.Increasing D and Y1 intensifies the separation of the film shear layer,leading to the formation of larger-scale kidney-shaped vortices.For all models,the streamwise h/h0 ranges from 3.1 to 5.2 within the in-terval 0<X<20 mm,and stabilizes between 1.5 and 2.1 while in the region X=30~60 mm,indicating the effective isolation of hot gases by the film layer.In the spanwise edge region(Z=25~30 mm),the model with D=1.3 mm exhibits a peak h/h0 value of up to 2.4,which is approximately about 14.2%higher than the peak spanwise h/h0 of the model with D=0.8 mm.
李锦添;江平;王首佳;陈蓓蓓;甘天源;李海龙
南昌航空大学动力与能源学院,江西南昌 330063||南昌航空大学绿色通用航空动力江西省重点实验室,江西南昌 330063南昌航空大学动力与能源学院,江西南昌 330063||南昌航空大学绿色通用航空动力江西省重点实验室,江西南昌 330063南昌航空大学动力与能源学院,江西南昌 330063||南昌航空大学绿色通用航空动力江西省重点实验室,江西南昌 330063南昌航空大学动力与能源学院,江西南昌 330063||南昌航空大学绿色通用航空动力江西省重点实验室,江西南昌 330063北京航空航天大学杭州国际创新学院,浙江 杭州 311115南昌航空大学动力与能源学院,江西南昌 330063
航空航天
气膜冷却综合冷效流量系数表面传热系数比
film coolingoverall cooling effectivenessflow coefficientsurface heat transfer coefficient ratio
《机械与电子》 2026 (5)
6-15,10
江西省研究生创新专项资金项目(YC2024-S628)
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