AOTV Bluff Body Flow-Relaxation Algorithm
- 1 January 1985
- book chapter
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 16 references indexed in Scilit:
- A natural conservative flux difference splitting for the hyperbolic systems of gasdynamicsPublished by Springer Nature ,2008
- The use of the Riemann problem in finite difference schemesPublished by Springer Nature ,1989
- Two dimensional and axisymmetric heat transfer results with the CSCMupwind implicit algorithmPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Complete flowfields over low and wide angle AOTV conceptual configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Universal single level implicit algorithm for gasdynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Multi-dimensional formulation of CSCM - An upwind flux difference eigenvector split method for the compressible Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- A natural conservative flux difference splitting for the hyperbolic systems of gasdynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Conservative supra-characteristics method for splitting the hyperbolic systems of gasdynamics with computed boundaries for real and perfect gasesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Applications and generalizations of variational methods for generating adaptive meshesApplied Mathematics and Computation, 1982
- Calculation of supersonic viscous flow over delta wings with sharp subsonic leading edgesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978