Stall onset on aerofoils at low to moderately high Reynolds number flows

@article{Morris2013StallOO,
  title={Stall onset on aerofoils at low to moderately high Reynolds number flows},
  author={Wallace J. Morris and Zvi Rusak},
  journal={Journal of Fluid Mechanics},
  year={2013},
  volume={733},
  pages={439 - 472}
}
Abstract The inception of leading-edge stall on stationary, two-dimensional, smooth, thin aerofoils at low to moderately high chord Reynolds number flows is investigated by a reduced-order, multiscale model problem via numerical simulations. The asymptotic theory demonstrates that a subsonic flow about a thin aerofoil can be described in terms of an outer region, around most of the aerofoil’s chord, and an inner region, around the nose, that asymptotically match each other. The flow in the… 

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