Numerical Optimization of a Vaned Shroud Design for Increased Operability Margin in Modern Centrifugal Compressors
Author:
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://turbomachinery.asmedigitalcollection.asme.org/data/Journals/JOTUEI/28732/627_1.pdf
Reference17 articles.
1. Dawes, W. , 1988, “Development of a 3D Navier-Stokes Solver for All Types of Turbomachinery,” ASME Paper 88-GT-70.
2. Wadia, A. , 1997, “Inner Workings of Aerodynamic Sweep,” ASME Paper 97-GT-401.
3. Development of Controlled Diffusion Airfoils for Multistage Compressor Application
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