Calculation of multistage turbomachinery using steady characteristic boundary conditions
Author:
Affiliation:
1. NASA, Lewis Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-968
Reference26 articles.
1. Denton,J.D. "The CalculationofThreeDimensional Viscous Flow Through MultistageTurbomachines,"ASMEPaper 90-GT-19,June 1990.
2. Toward Improved Throughflow Capability: The Use of Three-Dimensional Viscous Flow Solvers in a Multistage Environment
3. Three-Dimensional Navier-Stokes Analysis of a Two-Stage Gas Turbine
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