Wake transitions and laminar separation bubble in the flow past an Eppler 61 airfoil

• Published in: Physics of fluids (1994) Vol. 31; no. 11
• Main Authors: Samuthira Pandi, Jawahar Sivabharathy, Mittal, Sanjay
• Format: Journal Article
• Language: English
• Published: Melville American Institute of Physics 01.11.2019
• Subjects: Aerodynamics; Computational fluid dynamics; Flow stability; Fluid dynamics; Fluid flow; Horseshoe vortices; Laminar wakes; Periodic variations; Physics; Reynolds stress; Separation; Shear layers; Simulation; Spatial distribution; Stress concentration; Structural stability; Three dimensional flow; Vortex shedding
• ISSN: 1070-6631; 1089-7666
• DOI: 10.1063/1.5113823

The flow past an Eppler 61 airfoil at 10° angle to the free-stream is investigated numerically for 100 ≤ Re ≤ 87 000. Vortex shedding is observed beyond Re ∼ 600 and three-dimensionality sets in at Re ∼ 1280.9 via the mode C instability and hairpin vortex structures that grow with an increase in Re. At larger Re, the shear layer vortices, arising from the instability of the separated shear layer, interact with the flow close to the airfoil and cause it to reattach. A Laminar Separation Bubble (LSB) forms at Re ∼ 20 000 and beyond. The airfoil experiences a very significant increase in the lift and a decrease in the drag at the formation of LSB. Although the flow is three-dimensional, the primary mechanism of the formation of LSB appears to be two-dimensional. The length of the LSB decreases with an increase in Re. The variation of the shear layer and primary wake frequency, with Re, is studied. Both follow the power law. However, the variation before and after the formation of LSB is quite different. Unlike the primary wake frequency, the shear layer frequency suffers a jump at the formation of LSB. Wake formation length (Lf), estimated via the spatial distribution of Reynolds stress, exhibits spanwise periodicity at the onset of three-dimensionality.