Effect of Geometric Variation of Root Fillet on the Flow Characteristic of a Transonic Compressor Rotor

Author:

Cui Weiwei,Liu Yuqiang,Liu Fusong,Ruan Changlong,Yang Laishun,Li Longting,Yao Fei,Wang Xinglu,Wang Cuiping

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Reference29 articles.

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2. Deburge L.L., The aerodynamic significance of fillet geometry in turbocompressor blade rows. Journal of Engineering for Gas Turbines and Power, 1980, 102(4): 984–993.

3. Li J.B., Li X., Ji L.C., Yi W.L., Zhou L., Use of blended blade and end wall method in compressor cascades: Definition and mechanism comparisons. Aerospace Science and Technology, 2019, 92: 738–749.

4. Hoeger M., Baier R.D., Muller R., Engber M., Impact of a fillet on diffusing vane end-wall flow structure. Proceedings of the 11th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, Hawaii, USA, 2006, ISROMAC-11.

5. Hoeger M., Schmidt-Eisenlohr U., Gomez S., Sauer H., Müller R., Numerical simulation of the influence of a bulb and a fillet on the secondary flow in a compressor cascade. TASK Quarterly, 2019, 6(1): 25–37.

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