摘要: A test was conducted on a model of the NACA 0012 airfoil section with a solidupper surface or a porous upper surface with a cavity beneath for passive venting. The purposes of the test were to investigate the aerodynamic character... 展开
作者 | Mineck, R. E. Hartwich, P. M. | ||
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原报告号 | N9624022 | 总页数 | 96 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aerodynamic characteristics Airfoil profiles Airfoils Angle of attack Machnumber Porosity Pressure distribution Reynolds number Upper surface blowing Wind tunnel tests Aerodynamic forces Cavities Creep properties Leading edges Porous materia |