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

DOI10.1007/978-3-540-74460-3_27zbMath1409.76038OpenAlexW1869676113MaRDI QIDQ3122253

Jochen Wild, Holger Dettmar

Publication date: 20 March 2019

Published in: Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM) (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/978-3-540-74460-3_27

zbMATH Keywords

lift coefficientaerodynamic performancewing sectionincrease Reynolds numbersuction peak

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Boundary-layer theory for compressible fluids and gas dynamics (76N20) Transition to turbulence (76F06)

Uses Software

• MEGAFLOW

Cites Work

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

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