Time-Split Finite-Volume Method for Three-Dimensional Blunt-Body Flow
- 1 November 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (11), 1478-1485
- https://doi.org/10.2514/3.50614
Abstract
No abstract availableThis publication has 23 references indexed in Scilit:
- Multishocked, Three-Dimensional Supersonic Flowfields with Real Gas EffectsAIAA Journal, 1973
- Numerical Solution for Three-Dimensional Inviscid Supersonic FlowAIAA Journal, 1972
- Three-dimensional flow calculation by the method of characteristics.AIAA Journal, 1967
- Three-Dimensional Flow around Blunt BodiesAIAA Journal, 1967
- Inverse solution of blunt-body flowfields at large angle of attack.AIAA Journal, 1967
- A time-dependent computational method for blunt body flows.AIAA Journal, 1966
- Finite-difference calculations for hydrodynamic flows containing discontinuitiesJournal of Computational Physics, 1966
- A direct method for calculation of the flow about an axisymmetric blunt body at angle of attack.AIAA Journal, 1966
- Systems of conservation lawsCommunications on Pure and Applied Mathematics, 1960
- Weak solutions of nonlinear hyperbolic equations and their numerical computationCommunications on Pure and Applied Mathematics, 1954