Computation of supersonic turbulent flows over an inclined ogive-cylinder-flare
- 14 July 1980
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Numerical simulation of steady supersonic flow over an ogive-cylinder-boattail bodyPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Numerical solution of supersonic laminar flow over an inclined body of revolutionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Thin-layer approximation and algebraic model for separated turbulentflowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- A numerical method for solving the Navier-Stokes equations with application to shock-boundary layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Viscous flow over a cone at moderate incidence. Part 2. Supersonic boundary layerJournal of Fluid Mechanics, 1973