Establishing two-dimensional flow in a large-scale planar turbine cascade-Reference-Cited by-同舟云学术

Establishing two-dimensional flow in a large-scale planar turbine cascade

Published:1992-07-06 Issue: Volume: Page:
ISSN:
Container-title:28th Joint Propulsion Conference and Exhibit
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Author:

RODGER P.¹,SJOLANDER S.¹,MOUSTAPHA S.²

Affiliation:

1. Carleton University, Ottawa, Canada

2. Pratt & Whitney Canada, Longueuil

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3066

Reference11 articles.

1. Ilyas, M., and Norhury, J.F., 1973, "Effectof Axial Velocity Variation on the SubsonicFlow Through a Compressor Cascade," Inst. Mech. Engr., Paper C118/73.

2. Ohuonu,E.H., and Shaw, R., 1973, "Effectof Axial Velocity Variation on Deviation for CompressorCascades," Inst. Mech. Engr., Paper C53/73.

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