Modeling and Simulation of Unsteady Flow in Multistage Compressors Using Interdomain Boundaries
Author:
Affiliation:
1. Georgia Institute of Technology, Atlanta, Georgia 30332
2. Honeywell International, Inc., Phoenix, Arizona 85034
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B38414
Reference20 articles.
1. SchmidtJ. F. “Off-Design, Computer Code for Calculating the Aerodynamic Performance of Axial Flow Fans and Compressors,” NASA CR-198362, July 1995.
2. JohnsonM. S. “One-Dimensional, Stage-by-Stage, Axial Compressor Performance Model,” American Soc. of Mechanical Engineers Paper 91-GT-192, June 1991. 10.1115/91-GT-192
3. VeresJ. P. “Axial and Centrifugal Compressor Mean-Line Flow Analysis Method,” AIAA Paper 2009-1641, Jan. 2009. 10.2514/6.2009-1641
4. Surge and Rotating Stall in Axial Flow Compressors—Part I: Theoretical Compression System Model
5. The Stability of Pumping Systems—The 1980 Freeman Scholar Lecture
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