Acceleration of convergence to a periodic steady state in turbomachinery flows
Author:
Affiliation:
1. Stanford Univ., CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-152
Reference17 articles.
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2. Integration of Navier-Stokes equations using dual time stepping and a multigrid method
3. 3R.L. Davis, T. Shang, J. Buteau, and R. Ni. Prediction of 3-d Unsteady Flow in Multi-Stage Turbomachinery using an Implicit Dual Time-Step Approach. Technical Report 96-2565, AIAA, ASME, SAE, and ASEE 32nd Joint Propulsion Conference and Exhibit, Lake Buena Vista, FL, July 1996.
4. 4J. Yao, A.Jameson, J.J.Alonso, and F. Liu. Development and Validation ofa Massively Parallel Flow Solver forTurbomachinery Flows. Technical Report 00-0882, AIAA 38th Aerospace Sciences Meeting and Exhibit, January 2000.
5. Linearized Euler predictions of unsteady aerodynamic loads in cascades
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