Turbulent flow predictions for afterbody/nozzle geometries includingbase effects
- 1 May 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 7 (3) , 396-403
- https://doi.org/10.2514/3.23340
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- A method for calculating axisymmetric afterbody flowsJournal of Propulsion and Power, 1987
- Supersonic Axisymmetric Flow over Boattails Containing a Centered Propulsive JetAIAA Journal, 1984
- Computation of high Reynolds number internal/external flowsAIAA Journal, 1983
- Predictions of Channel and Boundary-Layer Flows with a Low-Reynolds-Number Turbulence ModelAIAA Journal, 1982
- A nonreflecting outflow boundary condition for subsonic navier-stokes calculationsJournal of Computational Physics, 1980
- Numerical Solution for Supersonic Turbulent Flow over a Compression RampAIAA Journal, 1975