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January 21, 2010, 02:47 |
NACA - Inclined flow / symmetryPlane
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Member
Stefan
Join Date: Jan 2010
Location: Kiel, Germany
Posts: 81
Rep Power: 16 |
Hello folks,
i investigate some elementary hydrodynamics using i.e. NACA profiles. The following illustration shows the case in 2D: Code:
OUTLET _________________________ |domain | | | | | s | | y | #| m | ##| m | ##| e S | ###| t I | ###| r D | ####| y E | ####| P | ####| l | ####| a | ####| n | ####| e | ###| | | |_______________________| INLET / / / / / / / / / / / / inclined flow My question/problem: When i want a specified angle fo attack, what is the direction of the flow on the reflected INLET (domain)? I guess the inclined flow is mirrored, too. Is there a possibility to maintain the inclined flow direction in case of that (e.g. that only the geometry/mesh will be duplicate, not the physical boundaries, maybe the mirrorMesh utility could help)? thx, /Stefan |
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airfoil, inclined flow, naca, symmetryplane |
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