General Equation Set Solver for Compressible and Incompressible Turbomachinery Flows
Author:
Affiliation:
1. Boston University
2. NASA Marshall Space Flight Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-4420
Reference6 articles.
1. Unsteady analysis of hot streak migration in a turbine stage
2. Roe,P.L."ApproximateRiemannSolvers,Parameter Vectors, and Difference Schemes,''Journalof ComputationalPhysics, Vol43, No. 2, 1981,pp.357-372.
3. Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods
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