Study on Part Clearance Flow Field for Variable Area LP Turbine Nozzle Vane using Different Turbulence Models
Author:
Affiliation:
1. Department of Aerospace Engineering, Indian Institute of Technology, Kharagpur, West Bengal, India 721302
Publisher
Gas Turbine Society of Japan
Link
https://www.jstage.jst.go.jp/article/jgpp/15/3/15_vol15no3tp14/_pdf
Reference36 articles.
1. Roy-Aikins, J. E. A., 1987, “A Study of Variable Geometry in Advanced Gas Turbines,” Ph.D Thesis, Cranfield Institute of Technology.
2. Roy-Aikins, J. E. A., 1990, “Considerations for the Use of Variable Geometry in Gas Turbines,” Proc. ASME Turbo Expo 1990, Vol. 5, Brussels, Belgium.
3. Aleid, L., 1997, “Variable Cycle Propulsion Systems for a Supersonic Civil Transport,” Ph.D Thesis, Cranfield Institute of Technology.
4. Bringhenti, C., and Barbosa, J. R., 2004, “Methodology for Gas Turbine Performance Improvement Using Variable- Geometry Compressors and Turbines,” Proc. Inst. Mech. Eng., Part A: J. Power Energy, Vol. 218(7), pp. 541–549.
5. Cumpsty, N. A., and Greitzer, E. M., 2004, “Ideas and Methods of Turbomachinery Aerodynamics :,” J. Propuls. Power, Vol. 20(1), pp. 15–26.
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