Applications of an unstructured solver to reactive, multiphase plume/propulsive flowfields
Author:
Affiliation:
1. Combustion Research and Flow Technology, Inc., Dublin, PA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2955
Reference19 articles.
1. Applications of an implicit, upwind Navier-Stokes code, CRAFT, to steady/unsteady reacting, multi-phase flowfields
2. Progress towards the analysis of transient combusting, multiphase flows using upwind/implicit numerics
3. Higher order solution of the Euler equations on unstructured grids using quadratic reconstruction
4. Numerical aspects of computing high Reynolds number flows on unstructured meshes
5. A 3-D upwind Euler solver for unstructured meshes
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1. Extension of unstructured hybrid grid method to supersonic combustion flows;37th Aerospace Sciences Meeting and Exhibit;1999-01-11
2. Scramjet inlet flow computations by hybrid grid method;36th AIAA Aerospace Sciences Meeting and Exhibit;1998-01-12
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