Numerical prediction of subsonic turbulent flows over slender bodiesat high incidence
- 1 December 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 29 (12) , 2054-2061
- https://doi.org/10.2514/3.10841
Abstract
No abstract availableKeywords
This publication has 18 references indexed in Scilit:
- Asymmetric turbulent vortical flows over slender bodiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Navier-Stokes computations of prolate spheroids at angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- A numerical study of three-dimensional separated flow past a hemisphere cylinderPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Computation of turbulent supersonic flows around pointed bodies having crossflow separationJournal of Computational Physics, 1986
- Computation of supersonic viscous flows around pointed bodies at large incidencePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- The complex asymmetric flow over a 3.5D ogive nose and cylindrical afterbody at high angles of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methodsJournal of Computational Physics, 1981
- Numerical Simulation of Steady Supersonic Viscous FlowAIAA Journal, 1980
- Implicit Finite-Difference Simulation of Flow about Arbitrary Two-Dimensional GeometriesAIAA Journal, 1978
- Calculation of compressible adiabatic turbulent boundary layersAIAA Journal, 1970