Vortical flow solutions using a time-lagged, thin-layer, Navier-Stokes algorithm
- 1 June 1991
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 29 (6) , 876-877
- https://doi.org/10.2514/3.10672
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Choice of implicit and explicit operators for the upwind differencing methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Time-accurate Euler equations solutions on dynamic blocked gridsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- An implicit, upwind, finite-volume method for solving the three-dimensional, thin-layer Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Approximate Riemann solvers, parameter vectors, and difference schemesJournal of Computational Physics, 1981
- Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methodsJournal of Computational Physics, 1981