Analysis of transitional separation bubbles on infinite swept wings
- 1 March 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 25 (3) , 421-428
- https://doi.org/10.2514/3.9640
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Analysis of airfoil leading-edge separation bubblesAIAA Journal, 1984
- Analysis of airfoil transitional separation bubblesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Investigation of a Reattaching Turbulent Shear Layer: Flow Over a Backward-Facing StepJournal of Fluids Engineering, 1980
- Calculation of Laminar Separation Bubbles and Their Effect on Airfoil PerformanceAIAA Journal, 1980
- 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
- Effect of free stream turbulence on the turbulent boundary layerInternational Journal of Heat and Mass Transfer, 1974
- Practical calculations of transitional boundary layersInternational Journal of Heat and Mass Transfer, 1973
- Some properties of boundary layer flow during the transition from laminar to turbulent motionJournal of Fluid Mechanics, 1957
- Further solutions of the Falkner-Skan equationMathematical Proceedings of the Cambridge Philosophical Society, 1954