Assessment of modeling and discretization accuracy for high-speed afterbody flows
- 1 July 1991
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 7 (4) , 607-616
- https://doi.org/10.2514/3.23369
Abstract
No abstract availableThis publication has 23 references indexed in Scilit:
- Theoretical analysis of aircraft afterbody flowJournal of Spacecraft and Rockets, 1987
- Accurate numerical simulation of supersonic jet exhaust flow with CSCM on adaptive overlapping gridsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Navier-Stokes calculations of rocket base flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Numerical simulation of axisymmetric base flow on tactical missiles with propulsive jetPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Numerical computation of base flow for a missile in the presence of a centered jetPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Predicting plume-induced separation on bluff-base bodiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Computation of a supersonic flow past an axisymmetric nozzle boattail with jet exhaustPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Numerical solution of axisymmetric boattail flow fields with plume simulatorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- An implicit finite-difference algorithm for hyperbolic systems in conservation-law formJournal of Computational Physics, 1976
- The numerical computation of turbulent flowsComputer Methods in Applied Mechanics and Engineering, 1974