NASA Low-Speed Centrifugal Compressor for 3-D Viscous Code Assessment and Fundamental Flow Physics Research
Author:
Affiliation:
1. U.S. Army Aviation Systems Command, Cleveland, OH
2. NASA Lewis Research Center, Cleveland, OH
3. Sverdrup Technology, Inc., Cleveland, OH
Abstract
Publisher
American Society of Mechanical Engineers
Link
http://asmedigitalcollection.asme.org/GT/proceedings-pdf/doi/10.1115/91-GT-140/2400367/v001t01a054-91-gt-140.pdf
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Influence of definition of impeller-vaneless diffuser boundary on physical validity of numerical simulations of viscid flow in the vaneless diffuser of a centrifugal compressor: A short review of case studies;AIP Conference Proceedings;2017
2. Effects of Coriolis Force on Flow in Rotating Diffusers;AIAA Journal;1997-07
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