Numerical analysis on the oscillation of stall cells over a NACA 0012 aerofoil

DOI10.1016/j.compfluid.2018.08.016zbMath1410.76006OpenAlexW2888669281MaRDI QIDQ1615628

Dajun Liu, Takafumi Nishino

Publication date: 31 October 2018

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: http://dspace.lib.cranfield.ac.uk/handle/1826/13553

zbMATH Keywords

proper orthogonal decompositionflow separationunsteady RANS2D-3D transitionlift fluctuation

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Software, source code, etc. for problems pertaining to fluid mechanics (76-04)

Related Items (1)

Link between subsonic stall and transonic buffet on swept and unswept wings: from global stability analysis to nonlinear dynamics

Cites Work

• On the birth of stall cells on airfoils
• Numerical study of airfoil stall cells using a very wide computational domain
• Structural changes of laminar separation bubbles induced by global linear instability
• Closed-loop control of an open cavity flow using reduced-order models
• A turbulent jet in crossflow analysed with proper orthogonal decomposition
• Turbulence and the dynamics of coherent structures. I. Coherent structures
• Low-order modelling of laminar flow regimes past a confined square cylinder
• Investigation of flow over an oscillating airfoil

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