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静叶栅上游端壁双射流气膜冷却特性实验
引用本文:雷蒋,鲁瑞山,秦岭,罗丁,何建宏,马元.静叶栅上游端壁双射流气膜冷却特性实验[J].火箭推进,2020,46(2):36-43.
作者姓名:雷蒋  鲁瑞山  秦岭  罗丁  何建宏  马元
作者单位:西安交通大学 机械结构强度与振动国家重点实验室,陕西 西安710049,西安交通大学 机械结构强度与振动国家重点实验室,陕西 西安710049,西安交通大学 机械结构强度与振动国家重点实验室,陕西 西安710049,西安交通大学 机械结构强度与振动国家重点实验室,陕西 西安710049,西安交通大学 机械结构强度与振动国家重点实验室,陕西 西安710049,西安航天动力研究所 陕西 西安710100
基金项目:高等学校学科创新引智计划计划);西安市科技计划;国家自然科学基金
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。

关 键 词:气膜冷却  双射流  静叶栅  压力敏感漆  吹风比  密度比

Experimental study of film-cooling characteristics of DJFC holes located upstream of a vane
LEI Jiang,LU Ruishan,QIN Ling,LUO Ding,HE Jianhong,MA Yuan.Experimental study of film-cooling characteristics of DJFC holes located upstream of a vane[J].Journal of Rocket Propulsion,2020,46(2):36-43.
Authors:LEI Jiang  LU Ruishan  QIN Ling  LUO Ding  HE Jianhong  MA Yuan
Institution:(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)
Abstract: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.
Keywords:film-cooling  DJFC  vane cascade  PSP  blowing ratio  density ratio
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