摘要
对燃烧室内开有发散孔的纵向波纹隔热屏进行了数值模拟.研究隔热屏的四种结构参数开孔率、波纹板高度、孔径和冷却通道高度的改变对隔热屏冷却效果的影响.研究表明:在气膜孔出流总量相同的情况下,3%开孔率比6%开孔率的隔热屏平均冷却效率较高;波纹板高度对隔热屏冷却效果影响较大,波纹板无量纲高度为1%比波纹板无量纲高度为2%和3.33%的隔热屏平均冷却效率高;孔径和冷却通道高度的改变对隔热屏冷却效果几乎没有影响.
The numerical simulation was used to study the effusion holes on the longitu dinal wavy liner in the combustor. The investigation focused on the parameters affecting cooling effectiveness, including: opening ratio, height of ripple hoard, diameter of holes and height of cooling passage. Given the same total flow effusion from holes, the results show that the heat shield gets a higher average cooling effectiveness when the opening ratio is 3 % compared with 6%; cooling effectiveness is sensitive to the height of ripple hoard, the heat shield gets the highest cooling effectiveness when the dimensionless height of ripple board is 1% compared with 2% and 3.33%; but there is a little influence on the cooling effectiveness of the liner with the change of the diameter of holes and the height of cooling passage.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2009年第1期18-24,共7页
Journal of Aerospace Power
关键词
波纹隔热屏
冷却效率
气膜冷却
数值模拟
发散孔
wavy liner
cooling effectiveness
film cooling
numerical simulation
effusion hole