Influences of Root Fillet and Dihedral Angle of Bowed Stator Blade on Aerodynamic Performance of Low-Speed Single-Stage Axial Compressor
Author:
Affiliation:
1. Division of Mechanical Engineering, Tokyo Denki University
2. Hosei University
Publisher
Gas Turbine Society of Japan
Link
https://www.jstage.jst.go.jp/article/jgpp/15/3/15_vol15no3tp07/_pdf
Reference15 articles.
1. Hewkin-Smith, M., Pullan, G., Grimshaw, S., Greitzer, E., and Panofsky, Z., 2019, “The role of tip leakage flow in spiketype rotating stall inception,” ASME J. Turbomachine., Vol.141, No. 6, pp. 061010-1–061010-10.
2. Yamada, K., Furukawa, M., Tamura, Y., Saito, S., Matsuoka, A., and Nakayama, K., 2017, “Large-scale detached eddy simulation analysis of stall inception process in a multistage axial flow compressor,” ASME J. Turbomach., Vol. 139, No. 7, pp. 071002-1–071002-11.
3. Lei, V., Spakovszky, Z. S., and Greitzer, E. M., 2008, “A Criterion for Axial Compressor Hub-Corner Stall,” ASME. J. Turbomach., Vol. 130, No. 3, pp. 031006-1–031006-10.
4. Xia, G., Medic, G., and Praisner, T. J., 2018, “Hybrid RANS/LES Simulation of Corner Stall in a Linear Compressor Cascade,” ASME J. Turbomach., Vol. 140, No. 8, pp. 081004-1–081004-11.
5. Dawkins, I., Taylor, J., Ottavy, X., and Miller, R., 2022, “The Unsteady Topology of Corner Separations,” ASME J. Turbomach., Vol. 144, No. 11, pp. 111001-1–111001-14.
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