An unconditionally stable Runge-Kutta method for unsteady flows
Author:
Affiliation:
1. NASA, Lewis Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-205
Reference22 articles.
1. Navier-Stokes simulations of rotor-stator interaction using patched and overlaid grids
2. Gibeling, H.J., Weinberg,B.C., Shamroth, S.J.,Mc-Donald, H. "Flow Through a Compressor Stage," AFOSR Report R86-910004-F, May 1986.
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