An analytical model of axisymmetric afterbody flow separation
- 20 January 1975
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Use of Coles' universal wake function for compressible turbulent boundary layersJournal of Aircraft, 1970
- An approach to turbulent incompressible separation under adverse pressure gradientsJournal of Aircraft, 1965
- The prediction of separation of the turbulent boundary layerJournal of Fluid Mechanics, 1959