Impeller-Diffuser Interaction in Centrifugal Compressors: Numerical Analysis of Radiver Test Case
Author:
Affiliation:
1. University of Florence, 50012 Florence, Italy
2. General Electric Oil & Gas, Nuovo Pignone, 50127 Florence, Italy
3. Sergio Stecco Department of Energy Engineering, University of Florence, 50139 Florence, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.27028
Reference30 articles.
1. Development of Secondary Flow Field in a Low Solidity Diffuser in a Transonic Centrifugal Compressor Stage
2. Aerodynamics of a Transonic Centrifugal Compressor Impeller
3. Flow With Shock Waves in a Transonic Centrifugal Compressor With a Low-Solidity Cascade Diffuser Using PIV
4. Detailed Flow Study of Mach Number 1.6 High Transonic Flow With a Shock Wave in a Pressure Ratio 11 Centrifugal Compressor Impeller
5. Impeller Blade Unsteady Aerodynamic Response to Vaned Diffuser Potential Fields
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