Prediction of attachment line transition for a high-lift wing based on two-dimensional flow calculations with RANS-solver

DOI10.1007/978-3-540-33287-9_25zbMath1323.76068OpenAlexW1581734409MaRDI QIDQ3196466

Joehen Wild, Oliver T. Schmidt

Publication date: 29 October 2015

Published in: New Results in Numerical and Experimental Fluid Mechanics V (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/978-3-540-33287-9_25

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) General aerodynamics and subsonic flows (76G25)

Related Items (1)

Manipulation of Attachment Line Transition by Geometry Modification at the Slat of a Multi-element Airfoil

Uses Software

• MEGAFLOW

Cites Work

• Simulation of three-dimensional symmetric and asymmetric instabilities in attachment-line boundary layers
• Simulation of nonlinear instabilities in an attachment-line boundary layer

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