Stabilization of Explicit Flow Solvers Using a Proper-Orthogonal-Decomposition Technique
Author:
Affiliation:
1. Department of Mechanical, Aerospace and Biomedical Engineering, University of Tennessee, Knoxville, Tennessee 37996-2030
2. Department of Mechanical Engineering and Materials Science, Duke University, Durham, North Carolina 27708-0300
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051945
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1. Calculation of unsteady flows in turbomachinery using the linearizedEuler equations
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4. A Time-Linearized Navier–Stokes Analysis of Stall Flutter
5. Linearized Unsteady Viscous Turbomachinery Flows Using Hybrid Grids
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