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静叶栅上游端壁双射流气膜冷却特性实验 被引量:3

Experimental study of film-cooling characteristics of DJFC holes located upstream of a vane
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摘要 为了进一步挖掘上游端壁气膜冷却的潜力,在低速叶栅风洞的静叶片上游端壁上,实验研究了双射流构型的气膜冷却特性,并与双排圆孔进行了对比。探究了吹风比(M=0.5,1.0,1.5,2.0)、密度比(Rd=1.0,1.5)的效应。端壁表面的气膜冷却效率通过压力敏感漆(PSP)测得。结果表明,吹风比的增大虽然会加剧吹离现象,但同时也会促进叶栅通道中、后段的气膜覆盖。密度比的增大会抑制气膜吹离,促进气膜横向覆盖和提高平均冷却效率。双射流孔相比于圆形孔,冷却气流在孔下游形成了反肾形涡,较好抑制了气膜吹离;但从双射流孔喷出的冷却气流对于叶栅通道内的涡系也更加敏感。在高吹风比下,双射流孔的冷却效率相对于圆形孔有一定的优势,特别是双射流I构型。 To further explore the potential of film-cooling on the upstream endwall,the film-cooling characteristics of DJFC(double-jet film-cooling)holes on the endwall upstream of a vane cascade was studied by experiments and corresponding results were compared with double-row streamwise cylindrical holes located in the same position.Effects of blowing ratio and density ratio were discussed.PSP(pressure sensitive paint)was applied to measure film-cooling effectiveness on the endwall.Results show,though increased blowing ratio induces film lift-off,film coverage on the mid-and rear-portion of the endwall improves.Increased density ratio suppresses lift-off,enhances lateral coverage and increases lateral-average of effectiveness.Compared to SC(streamuise cylindrical)holes,anti-kidney vortices form at the exit of DJFC holes and thus decreases lift-off.However,DJFC holes are more sensitive to vortices generated in the cascade passage.At high blowing ratios,film effectiveness of DJFC holes are more advantageous over SC holes,especially DJFC I.
作者 雷蒋 鲁瑞山 秦岭 罗丁 何建宏 马元 LEI Jiang;LU Ruishan;QIN Ling;LUO Ding;HE Jianhong;MA Yuan(State Key Laboratory for Strength and Vibration of Mechanical Structures,Xi'an Jiaotong University,Xi'an 710049,China;Xi'an Aerospace Propulsion Institute,Xi'an 710100,China)
出处 《火箭推进》 CAS 2020年第2期36-43,共8页 Journal of Rocket Propulsion
基金 国家自然科学基金(51776153) 111引智项目(B18040) 西安市科技计划项目(201805034YD12CG18(3))。
关键词 气膜冷却 双射流 静叶栅 压力敏感漆 吹风比 密度比 film-cooling DJFC vane cascade PSP blowing ratio density ratio
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