New, quasi-simultaneous method to calculate interacting boundary layers
- 1 January 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 19 (1) , 79-85
- https://doi.org/10.2514/3.7748
Abstract
No abstract availableThis publication has 21 references indexed in Scilit:
- Calculation of separated flows at subsonic and transonic speedsPublished by Springer Nature ,2007
- Laminar boundary layers with assigned wall shearPublished by Springer Nature ,2007
- Prediction of Incompressible Separated Boundary Layers Including Viscous-Inviscid InteractionJournal of Fluids Engineering, 1979
- A new boundary-layer inviscid iteration technique for separated flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Incompressible Boundary-Layer SeparationAnnual Review of Fluid Mechanics, 1977
- Solutions of the Navier–Stokes Equation at Large Reynolds NumberSIAM Journal on Applied Mathematics, 1975
- Solutions for laminar boundary layers with separation and reattachmentPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- On laminar boundary-layer separationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Laminar SeparationAnnual Review of Fluid Mechanics, 1969
- The integration of the two-dimensional laminar boundary-layer equations past the point of vanishing skin frictionJournal of Fluid Mechanics, 1966