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Simulation of 3D unsteady incompressible flow past a NACA 0012 wing section
KTH, School of Computer Science and Communication (CSC), Numerical Analysis, NA (closed 2012-06-30). (Computational Technology Laboratory)ORCID iD: 0000-0002-1695-8809
KTH, School of Computer Science and Communication (CSC), Numerical Analysis, NA (closed 2012-06-30). (Computational Technology Laboratory)ORCID iD: 0000-0003-4256-0463
KTH, School of Computer Science and Communication (CSC), Numerical Analysis, NA (closed 2012-06-30). (Computational Technology Laboratory)ORCID iD: 0000-0002-5020-1631
2012 (English)Report (Other academic)
Abstract [en]

We present computational simulations of three-dimensional unsteady high Reynolds number incompressible flow past a NACA 0012 wing profile, for a range of angles of attack, from low lift through stall. A stabilized finite element method is used, referred to as General Galerkin (G2), with adaptive mesh refinement with respect to the error in target output, such as aerodynamic forces. Computational predictions of aerodynamic forces are validated against experimental data.

Place, publisher, year, edition, pages
Stockholm: KTH Royal Institute of Technology, 2012. , 13 p.
Series
TRITA-CTL-4, 023
National Category
Computational Mathematics
Identifiers
URN: urn:nbn:se:kth:diva-95389OAI: oai:DiVA.org:kth-95389DiVA: diva2:528062
Funder
Swedish e‐Science Research Center
Note

QC 20120913

Available from: 2012-05-23 Created: 2012-05-23 Last updated: 2013-04-09Bibliographically approved

Open Access in DiVA

fulltext(19807 kB)2101 downloads
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Type fulltextMimetype application/pdf

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Jansson, JohanHoffman, JohanJansson, Niclas
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CiteExportLink to record
Permanent link

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Citation style
  • apa
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf