Flow simulation of NAL experimental supersonic airplane/booster separation using overset unstructured grids
- 1 July 2001
- journal article
- Published by Elsevier BV in Computers & Fluids
- Vol. 30 (6), 673-688
- https://doi.org/10.1016/s0045-7930(00)00033-5
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Direct surface triangulation using stereolithography (STL) dataPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2000
- An intergrid-boundary definition method for overset unstructured grid approachPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- Reordering of Hybrid Unstructured Grids for Lower-Upper Symmetric Gauss-Seidel ComputationsAIAA Journal, 1998
- Coverage acceleration of an aeroelastic Navier-Stokes solverPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- On the accuracy of limiters and convergence to steady state solutionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Lower-upper implicit schemes with multiple grids for the Euler equationsAIAA Journal, 1987
- A 3-D chimera grid embedding techniquePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985