Volume -I , Issue -VI, August 2014

FINITE ELEMENT ANALYSIS ON AXIAL COMPRESSOR BLADE

Author(s) :

Shruthi J. H. , Ravi Kiran B. S.v

Abstract

Compressor is one of the most important part in gas turbine. The compressor has compressor blades which compress the gas which flows from the inlet and leaves the gas with higher temperature and pressure to the outlet. The project is to design and analysis of compressor blade. CATIA is used to design the solid model and ANSYS for analysis for Finite Element model generation by applying boundary condition which also includes specific post-processing and life assessment of the blade. However the program makes effective use of the ANSYS Pre-processor to mesh complex compressor blade geometries and apply boundary conditions. The objective of the current task is to perform the Static and Dynamic (modal) analysis to know the stress and strain at the high temperature zone.

Keywords

Compressor blade, Design, CATIA, ANSYS, Static analysis, Dynamic analysis.

References
  1. Wilson, E.L., "Structural Analysis of Axisymmetric Solids", AIAA Journal, Volume 3, No.12, December 1965.
  2. Aero0015-1 - mechanical design of turbomachinery - 5 ects - j.-c.golinval – University of Liege (Belgium).
  3. Skubbaachevskiy, G.S. Aviation gas turbine engines, construction and design of parts. Foreign Technology Edition. 1969.
  4. A. H. Shapiro, The Dynamics and Thermodynamics of Compressible Fluid Flow, Ronald Press, New York (1954).
  5. Roark, R.J., "Formulas For Stress and Strain", McGraw-Hill, 1965.
  6. E. R. C. Eckert and R. M. Drake, Analysis of Heat and Mass Transfer, McGraw-Hill, New York (1972).
  7. F. P. Incropera and D. P. DeWitt, Fundamentals of Heat and Mass Transfer, 2nd ed. J. Wiley & Sons, New York (1985).
How to Cite this Paper? [APA Style]
Shruthi J. H. , Ravi Kiran B. S.v, (2014), FINITE ELEMENT ANALYSIS ON AXIAL COMPRESSOR BLADE, Industrial Science Journal, http://industrialscience.org/Article.aspx?aid=46&vid=6, (August, 2014)
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