The use of sweep and dihedral in multistage axial flow compressor blading - Part II: Low and high-speed designs and test verification

Journal of Turbomachinery

Volumn 124, Issue 4, 2002, Pages 533-542

  Gallimore, Simon J ^a   Bolger, John J ^a   Cumpsty, Nicholas A ^a   Taylor, Mark J ^b   Wright, Peter I ^b   Place, James M M ^b  

^a ASME   (United Kingdom)

^b ROLLS ROYCE PLC   (United Kingdom)

Author keywords

Compressor; Design; Dihedral; Multistage; Sweep

Indexed keywords

AXIAL FLOW; COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; MACHINE DESIGN; ROTORS; TURBOMACHINE BLADES;

MULTISTAGE AXIAL FLOW;

HIGH PRESSURE TURBOMACHINERY;

AXIAL FLOW COMPRESSOR; BLADE; DESIGN; RESEARCH AND DEVELOPMENT; TESTING;

EID: 0036820583     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1507334     Document Type: Article

References (3)

1. Gallimore, S. J., Bolger, J. J., Cumpsty, N. A., Taylor, M. J., Wright, P. I., and Place, J. M. M., 2002, "The Use of Sweep and Dihedral in Multistage Axial Flow Compressor Blading Part I: University Research and Methods Development," ASME J. Turbomach., 124, pp. 521-532.
2. Howard, M. A., Ivey, P. C., Barton, J. P., and Young, K. F., 1994, "Endwall Effects at Two Tip Clearances in a Multistage Axial Flow Compressor with Controlled Diffusion Blading," ASME J. Turbomach., 116, pp. 635-647.
3. Swoboda, M., Ivey, P. C., Wenger, U., Gümmer, V., 1998, "An Experimental Examination of Cantilevered and Shrouded Stators in