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鱼鳞纹叶栅试验研究
引用本文:苗润田,王连贵,高歌.鱼鳞纹叶栅试验研究[J].航空动力学报,1998,13(1):27-29,105.
作者姓名:苗润田  王连贵  高歌
作者单位:1.沈阳黎明发动机制造公司
摘    要:鱼鳞纹叶栅临界马赫数比原型提高了9.5%,减少了46.9%,比直纹叶栅也减少了10.7%。最大二元静压比比原型高2.7%,比直纹叶栅高1.17%。在原型叶栅不能达到的Ma1=0.8处,两种花纹叶栅均未堵塞。

关 键 词:压气机    叶栅    减阻    试验
收稿时间:1996/12/1 0:00:00
修稿时间:5/1/1997 12:00:00 AM

EXPERIMENTAL INVESTIGATION OF FISH SCALE PATTERNED CASCADE
Miao Runtian an,Wang Liangui and Gao Ge.EXPERIMENTAL INVESTIGATION OF FISH SCALE PATTERNED CASCADE[J].Journal of Aerospace Power,1998,13(1):27-29,105.
Authors:Miao Runtian an  Wang Liangui and Gao Ge
Institution:1.Design Dept.Shenyang LIMING Engine Manufacturing Co.,Shenyang 1100432.4th Dept.Beijing University of Aeronautics and Astronautics,Beijing 100083
Abstract:Several cascades with different patterns have been tested with the purpose of turbulence drag reduction in compressor cascade,after the straight patterned cascade obtained notable effects.The fish scale patterned cascade is the best of them.The main performance comparison is shown as follows: CascadeMa1cr△βdesignδdesign(P2/P1)2Dmaxξi=05°/%△ireference straight pattern fish scale pattern0685 0735 0750408° 417° 411°67° 58° 64°11810 11987 1212757609 34261 30610100° 104° 104° The above test data indicate that most of performance indices of the fish scale patterned cascade,such as critical Mach number Ma1cr,maximum two-dimensional static compression ratio (P2/P1)2Dmax and total pressure loss coefficient at maximum attack angle ξi=05° are improved over the straight patterned cascade.The other performance parameters,namely attack angle range △i,flow deflection angle at design point △βdesign and corresponding deviation angle at design point δdesign,are superior to the reference cascade as well.It is particularly worth to point out that the fish scale pattern and the straight pattern can be together applied to the same blade to obtain advantageous performance. 
Keywords:Compressors cascades  Drag reduction  Experiment
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