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NACA0012
Details of airfoil (aerofoil)(n0012-il) NACA 0012 AIRFOILS NACA 0012 airfoil.
The turbulent NACA 0012 airfoil case should be run at essentially incompressible conditions (the recommendation here is to ...
NACA0012(来源:turbmodels.larc.nasa.gov)
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作者:大竹智久2007被引用次数:49 — Aerodynamic characteristics of NACA0012 airfoil at low Reynolds numbers (Re=1.0×104∼1.0×105) are measured systematically to clarify ...
作者:大竹智久2007被引用次数:49 — NACA0012 Aerofoil at Low Reynolds Numbers ... Abstract : Aerodynamic characteristics of NACA0012 airfoil at low Reynolds numbers (Re = 1.0 × 104.
作者:中谷淳2014被引用次数:1 — In this study, the reliability of OpenFOAM has been confirmed through the incompressible fluid analysis around the NACA0012 airfoil.
作者:I Rodríguez2013被引用次数:70 — At low-to-moderate Reynolds numbers, NACA0012 exhibits a combination of leading-edge/trailing-edge stall which causes the massive separation of the flow on the ...
作者:S Eftekhari2019被引用次数:9 — ABSTRACT: The aerodynamic characteristics of a NACA0012 wing geometry at low Reynold's numbers and angle of attack ranging from 0° to 90° are investigated ...
2010年4月6日 — The NACA 0012 airfoil is widely used. The simple geometry and the large amount of wind tunnel data provide ...
NACA0012(来源:www.cfd-online.com)
This test case is for the NACA 0012 in high Reynolds number flow. It has become a classic test case for RANS solvers due to ...
NACA0012(来源:su2code.github.io)

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