Numerical simulation of three-dimensional boattail afterbody flow fields
- 14 July 1980
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- Calculation of Separated Turbulent Flows on Axisymmetric Afterbodies Including Exhaust Plume EffectsAIAA Journal, 1980
- Implicit Finite-Difference Simulations of Three-Dimensional Compressible FlowAIAA Journal, 1980
- Numerical Solution of a Supersonic Nozzle Afterbody Flow with Jet ExhaustPublished by Defense Technical Information Center (DTIC) ,1979
- Simulation of three-dimensional compressible viscous flow on the Illiac IV computerPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Computation of a supersonic flow past an axisymmetric nozzle boattail with jet exhaustPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Analytical study of viscous effects on transonic flow over boattail nozzlesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- 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
- Model of the Engine Exhaust System at Transonic Flight SpeedsJournal of Spacecraft and Rockets, 1975
- Calculation of potential flow about arbitrary bodiesProgress in Aerospace Sciences, 1967