Control of leading-edge separation from an airfoil by internal acoustic excitation and self-induced resonances
Authors:
- 1 January 1999
- book chapter
- Published by Springer Nature
- p. 299-304
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Vortical structure morphology in the initial region of a forced mixing layer: roll-up and pairingJournal of Fluid Mechanics, 1996
- Control of wall-separated flow by internal acoustic excitationAIAA Journal, 1990
- Small-scale transition in a plane mixing layerJournal of Fluid Mechanics, 1990
- Separation control over an airfoil at high angles of attack by soundemanating from the surface1987
- Perturbed Free Shear LayersAnnual Review of Fluid Mechanics, 1984