Numerical Stability Conditions in the Calculation of Potential Velocity Fields
Author:
Affiliation:
1. Centre National de la Recherche Scientique, 75013 Paris, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.703
Reference21 articles.
1. The Application of Singularity Methods to Blade to Blade Calculations
2. Boundary element method for the analysis of the unsteady flow aroundextreme propeller geometries
3. Belamri, T. “Blade to Blade, Multicascades and Unsteady Flow Analysis by the Singularities Method. Application to Incompressible Flow Turbomachines,” Ph.D. Thesis,Dept. of Mechanical Engineering, cole Nationale Suprieure d’Arts et Mtiers, Paris, France, July 1998.
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1. Inverse Design Method for Centrifugal Impellers and Comparison with Numerical Simulation Tools;International Journal of Computational Fluid Dynamics;2004-02
2. On a General Method of Unsteady Potential Calculation Applied to the Compression Stages of a Turbomachine—Part I: Theoretical Approach;Journal of Fluids Engineering;2001-06-06
3. Calcul potentiel instationnaire appliqué à l'interaction roue-volute des pompes centrifuges;La Houille Blanche;2001-04-01
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