Three-Dimensional Unsteady Multi-stage Turbomachinery Simulations Using the Harmonic Balance Technique
Author:
Affiliation:
1. Stanford University
2. Duke University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-892
Reference28 articles.
1. Unsteady flow investigations in an axial turbine using the massively parallel flow solver TFLO
2. Development and Validation of a Massively Parallel Flow Solver for Turbomachinery Flows
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