摘要: The effects of potential in-flight ice accretion on the aerodynamic performance of a multi-element high-lift airfoil have been investigated at moderate-to-high Reynolds numbers. The investigation was conducted in the Low Turbulenc... 展开
作者 | Khodadoust, A. Dominik, C. Shin, J. Miller, D. | ||
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原报告号 | N19970008122 | 总页数 | 10 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Airfoils Aircraft icing Reynolds number Wind tunnel tests Angle of attack Lift Surface roughness Pressure distribution Leading edges Aircraft safety |