Analysis of airfoil leading-edge separation bubbles
- 1 December 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 22 (12) , 1697-1704
- https://doi.org/10.2514/3.8840
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- Low-speed flows involving bubble separationsPublished by Elsevier ,2003
- Prediction of Separating Turbulent Boundary Layers Including Regions of Reversed Flow.Published by Defense Technical Information Center (DTIC) ,1980
- An improved interaction method for exhaust nozzle boattail flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Calculation of Laminar Separation Bubbles and Their Effect on Airfoil PerformanceAIAA Journal, 1980
- A new boundary-layer inviscid iteration technique for separated flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Theory of viscous transonic flow over airfoils at high Reynolds numberPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Analysis of leading-edge separation bubbles on airfoilsAIAA Journal, 1976
- Numerical prediction of incompressible separation bubblesJournal of Fluid Mechanics, 1975
- The interaction of a shock wave with a laminar boundary layer†International Journal of Non-Linear Mechanics, 1968
- Some properties of boundary layer flow during the transition from laminar to turbulent motionJournal of Fluid Mechanics, 1957