摘要: In support of the NASA Lewis Modern Airfoils Ice Accretion Test Program, the University of Illinois at Urbana-Champaign provided expertise in airfoil design and aerodynamic analysis to determine the aerodynamic effect of ice accre... 展开
作者 | Selig, M. S. Bragg, M. B. Saeed, F. | ||
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原报告号 | N19980038243 | 总页数 | 25 |
主办者 | National Aeronautics and Space Administration, Washington, DC. | ||
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Aerodynamic characteristics Design analysis Airfoils Leading edges Ice formation Wings Aerodynamics |