2014
DOI: 10.1098/rsta.2013.0343
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On recent developments in marginal separation theory

Abstract: Thin aerofoils are prone to localized flow separation at their leading edge if subjected to moderate angles of attack α. Although ‘laminar separation bubbles’ at first do not significantly alter the aerofoil performance, they tend to ‘burst’ if α is increased further or if perturbations acting upon the flow reach a certain intensity. This then either leads to global flow separation (stall) or triggers the laminar–turbulent transition process within the boundary layer flow. This paper addresses the asymptotic a… Show more

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Cited by 19 publications
(11 citation statements)
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“…Scaling the innovation fits perfectly along the demand curve will even lead to revenue in the amount of the integral underneath the curve. To make this possible several methods of business informatics can be used to extract, collect and analyze data, emulating variability and evolutionary processes during product development and research processes [1,2,3].…”
Section: Plastic Part Solutions For Agile Industry Applicationmentioning
confidence: 99%
“…Scaling the innovation fits perfectly along the demand curve will even lead to revenue in the amount of the integral underneath the curve. To make this possible several methods of business informatics can be used to extract, collect and analyze data, emulating variability and evolutionary processes during product development and research processes [1,2,3].…”
Section: Plastic Part Solutions For Agile Industry Applicationmentioning
confidence: 99%
“…The uniform flow pattern around a fixed plate continues to be actively studied both experimentally [13,14] and theoretically with the aim of improving the methods of laminarization of flow on the wing and turbulence description [15]. Much attention is paid to analysis of the flow in the region of the boundary layer separation from the plate [16], as well as calculation of the velocity field taking into account the complex multilevel flow structure [17]. The boundary layer separation from a plate with a sharpened leading edge leads to the formation of a sequence of leading-edge vortices with their properties studied for several values of the angles of attack in [18].…”
Section: Introductionmentioning
confidence: 99%
“…Regularization methods in this regard were not yet known and moreover the computing power available at that time was still insufficient to solve the occasionally delicate nonlinear evolution equations numerically. Of course, high-end computing power is available now, and as far as the ill-posedness is concerned, we believe these difficulties can be overcome as well [ 28 ].…”
Section: Introductionmentioning
confidence: 99%