Quasi-3 dimensional analysis and design of turbomachinery blades

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Ekici, Kivanç ^a   Akmandor, I Sinan ^a   Çetinkaya, Tahsin ^a  

^a MIDDLE EAST TECHNICAL UNIVERSITY   (Turkey)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; ALGORITHMS; BOUNDARY LAYERS; RUNGE KUTTA METHODS; TURBOMACHINE BLADES; TURBOMACHINERY;

COMPUTATIONAL ACCURACY; COUPLED ALGORITHMS; FINITE VOLUME SCHEMES; MERIDIONAL PLANES; NEWTON-RAPHSON LINEARIZATION; PRELIMINARY DESIGN; QUASI 3-DIMENSIONAL ANALYSIS; QUASI THREE-DIMENSIONAL ANALYSIS;

MACHINE DESIGN;

EID: 84983171470     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. Giles, M. B and Drela, M 'Two-Dimensional Transonic Aerodynamic Design Method,' AIAA J., Vol. 25, No. 9, (September 1987) pp. 1199-1206.
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3. Giles, M. B. "Newton solution of steady twodimensional transonic flow." Ph. D. Thesis, Department of Aeronautics and Astronautics, MIT, (June 1985).
4. Drela, M., "Two-dimensional transonic aerodynamic design and analysis using the Euler equations." Ph. D. Thesis, Department of Aeronautics and Astronautics, MIT, (December 1985).
5. Cetinkaya, T. A., "2D and axisymmetric Euler solver for aerodynamic analysis and design." Ph. D. Thesis, Mechanical Engineering Department, Middle East Technical University, (June 1990).
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7. Uzol, O., "Quasi-three dimensional numerical design of turbomachinery blades." M. Sc. Thesis, Aeronautical Engineering Department, Middle East Technical University, (July 1995).
8. Ekici. K., "Quasi-three dimensional analysis and design of turbomachinery blades with boundary layer coupling." M. Sc. Thesis, Aeronautical Engineering Department, Middle East Technical University, (June 1997).
9. Gostelow, J. P., Cascade Aerodynamics, Pergamon Press, Oxford, (1984).
10. Dunker, R. J., "Test case E/CO-4 single transonic compressor stage" AGARD-AR-275, (1990), pp. 245-285.