A Three-Dimensional Boundary-Layer Method for Flow over Delta Wings with Leading-Edge Separation
- 1 October 1985
- proceedings article
- Published by SAE International
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- A physically optimum difference scheme for three-dimensional boundary layersPublished by Springer Nature ,2005
- A Three-Dimensional Boundary-Layer Method for Flow over Delta Wings with Leading-Edge SeparationPublished by SAE International ,1985
- Numerical and experimental determination of secondary separation on delta wings in subsonic flowJournal of Aircraft, 1985
- Time-dependent solution of three-dimensional compressible turbulent integral boundary-layer equationsAIAA Journal, 1985
- A vector-oriented finite difference scheme for calculating three-dimensional compressible laminar and turbulent boundary layers on practical wing configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- A Method for the Calculation of 3D Boundary Layers on Practical Wing ConfigurationsJournal of Fluids Engineering, 1981
- Finite-difference solution of the incompressible three-dimensional boundary layer equations for a blunt bodyComputers & Fluids, 1973
- On the determination of the zones of influence and dependence for three-dimensional boundary-layer equationsJournal of Fluid Mechanics, 1971
- Three-dimensional boundary layer near the plane of symmetry of a spheroid at incidenceJournal of Fluid Mechanics, 1970
- A Simple Laminar Boundary Layer with Secondary FlowJournal of the Aeronautical Sciences, 1955