摘要: An experimental study has been conducted to investigate ice accretions on a high-lift, multi-element airfoil in the Icing Research Tunnel at the NASA Lewis Research Center. The airfoil is representative of an advanced transport wi... 展开
作者 | Shin, Jaiwon Wilcox, Peter Chin, Vincent Sheldon, David | ||
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原报告号 | NASA-TM-106620 | 总页数 | 22 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | AIRCRAFT ICING AIRFOILS LIFT WIND TUNNEL TESTS AIRCRAFT DESIGN AIRCRAFT HAZARDS FLIGHT HAZARDS FLIGHT TESTS |