Efficient Edge-Based Rotor/Stator Interaction Method
Author:
Affiliation:
1. Universidad Politécnica de Cartagena, 30006 Murcia, Spain
2. Industria de Turbopropulsores, S. A., 28830 Madrid, Spain
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.44512
Reference28 articles.
1. Vibrations of Bladed-Disk Assemblies—A Selected Survey (Survey Paper)
2. BLADEROW INTERACTIONS, TRANSITION, AND HIGH-LIFT AEROFOILS IN LOW-PRESSURE TURBINES
3. Streamline Curvature Computing Procedures for Fluid-Flow Problems
4. A Quasi-Three-Dimensional Turbomachinery Blade Design System: Part I—Throughflow Analysis
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