Development of a Low Flow Coefficient Single Stage Centrifugal Compressor-Reference-Cited by-同舟云学术

Development of a Low Flow Coefficient Single Stage Centrifugal Compressor

Published:2009-06-19 Issue:4 Volume:10 Page:282-289
ISSN:1550-2287
Container-title:International Journal for Computational Methods in Engineering Science and Mechanics
language:en
Short-container-title:International Journal for Computational Methods in Engineering Science and Mechanics

Author:

Xu C.,Amano R. S.

Publisher

Informa UK Limited

Subject

Computational Mathematics,Computational Mechanics

Link

http://www.tandfonline.com/doi/pdf/10.1080/15502280902939460

Reference17 articles.

1. Investigation of an Axial Fan-Blade Stress and Vibration Due to Aerodynamic Pressure Field and Centrifugal Effects

2. Kenny, D. P. The History and Future of the Centrifugal Compressor in Aviation Gas Turbine. 1stCliff Garrett Turbomachinery Award Lecture, Society of Automotive Engineers. SAE/SP-804/602

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