Investigation of flow at leading and trailing edges of pitching-up airfoil
- 1 August 1995
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 33 (8) , 1369-1376
- https://doi.org/10.2514/3.12560
Abstract
No abstract availableThis publication has 18 references indexed in Scilit:
- Two-dimensional unsteady leading-edge separation on a pitching airfoilAIAA Journal, 1994
- Vortex Interactions with WallsAnnual Review of Fluid Mechanics, 1994
- Unsteady flow past an airfoil pitching at a constant rateAIAA Journal, 1992
- Unsteady pressure field and vorticity production over a pitching airfoilAIAA Journal, 1992
- Study of role of unsteady separation in formation of dynamic stall vortexPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Vortex-induced boundary-layer separation. Part 2. Unsteady interacting boundary-layer theoryJournal of Fluid Mechanics, 1991
- Dynamic stall of a constant-rate pitching airfoilJournal of Aircraft, 1990
- Progress in analysis and prediction of dynamic stallJournal of Aircraft, 1988
- Unsteady AirfoilsAnnual Review of Fluid Mechanics, 1982
- The spontaneous generation of the singularity in a separating laminar boundary layerJournal of Computational Physics, 1980