A new turbulence closure model for boundary layer flows with strong adverse pressure gradients and separation
- 9 January 1984
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Supercritical airfoil boundary-layer and near-wake measurementsJournal of Aircraft, 1983
- The structure of a separating turbulent boundary layer. Part 1. Mean flow and Reynolds stressesJournal of Fluid Mechanics, 1981
- The understanding and prediction of turbulent flowThe Aeronautical Journal, 1972
- Calculation of boundary-layer development using the turbulent energy equationJournal of Fluid Mechanics, 1967