The three-dimensional aerodynamic design and test of a three-stage transonic compressor r

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1999, Pages

  Li, Y S ^a   Wells, R G ^a  

^a ALSTOM   (France)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT ENGINES; COMPRESSIBILITY OF GASES; COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; GAS COMPRESSORS; GAS TURBINES; NAVIER STOKES EQUATIONS; SUPERSONIC AIRCRAFT; TRANSONIC AERODYNAMICS; TRANSONIC FLOW; TURBOMACHINE BLADES;

AERODYNAMIC DESIGNS; CONTROLLED DIFFUSION; CONVENTIONAL DESIGN; DESIGN SYSTEMS; DOUBLE CIRCULAR ARCS; MULTISTAGE COMPRESSOR; PRESSURE RATIO; TRANSONIC COMPRESSOR;

DESIGN;

EID: 84928563564     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/99-GT-068     Document Type: Conference Paper

References (4)

1. Carchedi, F., 1988, "Design and Development of the Ruston Typhoon Gas Turbine", ASME Cogen-Turbo, 2nd Int. Symposium on Turbomachinery & Cogeneration, Montreux, Switzerland, Aug. 1988, pp 101-109.
2. Dawes, W. N., 1988, "Development of a 3D Navier-Stokes Solver for Application to all Types of Turbomachinery", ASME Paper No. 88-01-70.
3. Denton, J. D., 1990, "The Calculation of Three Dimensional Viscous Flow Through Multistage Turbomachines", ASME Paper No. 90-GT-19.
4. Wells, R. G., Baty, G., Carchedi, F. and Wood, G. It, 1989, "The Design and Test of a Two Stage Transonic Axial Flow Compressor", ASME Paper No. 89-GT-164.