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Simulation of 3D un...
Simulation of 3D unsteady incompressible flow past a NACA 0012 wing section
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- Jansson, Johan, 1978- (författare)
- KTH,Numerisk analys, NA,Computational Technology Laboratory
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- Hoffman, Johan (författare)
- KTH,Numerisk analys, NA,Computational Technology Laboratory
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- Jansson, Niclas (författare)
- KTH,Numerisk analys, NA,Computational Technology Laboratory
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(creator_code:org_t)
- Stockholm : KTH Royal Institute of Technology, 2012
- Engelska 13 s.
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Abstract
Ämnesord
Stäng
- 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.
Ämnesord
- NATURVETENSKAP -- Matematik -- Beräkningsmatematik (hsv//swe)
- NATURAL SCIENCES -- Mathematics -- Computational Mathematics (hsv//eng)
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