SWIFT Code Assessment for Two Similar Transonic Compressors-Reference-Cited by-同舟云学术

SWIFT Code Assessment for Two Similar Transonic Compressors

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
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Author:

Chima Rodrick¹

Affiliation:

1. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-1058

Reference18 articles.

1. 2Reid,L.andMoore,R.D."PerformanceofaSingle-StageAxial-FlowTransonicCompressorwithRotorandStatorAspect Ratios of1.19and 1.26, Respectively,and withDesign Pressure Ratioof 1.82, NASA TP-1338, 1978.

2. Experimental Study of Low Aspect Ratio Compressor Blading

3. The Effect of Adding Roughness and Thickness to a Transonic Axial Compressor Rotor

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