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首页> 美国政府科技报告 >Experimental Study of the Aerodynamics of a NACA0012 Airfoil with a SimulatedGlaze Ice Accretion, Volume 2
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Experimental Study of the Aerodynamics of a NACA0012 Airfoil with a SimulatedGlaze Ice Accretion, Volume 2

机译：模拟釉冰吸收NaCa0012翼型空气动力学实验研究，第2卷

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This is the second volume of a report documenting the effect of simulated iceaccretion on the aerodynamic performance of a NACA 0012 airfoil. Both an experimentally measured and a computer generated ice shape are studied. The purpose of this report is to present the results of the measurements, not an analysis of the data. Surface pressure, integrated lift and pitching moment data are presented as well as drag from a wake survey. A split hot film probe was used to document the flow-field about the airfoil with simulated ice. Data in the separation bubbles, reattached boundary layer and wake are presented. Both tabulated and graphical data are presented in the paper. The data are also available on computer disk for easy access.

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