摘要: One-ninth scale wind tunnel model tests of the Propfan Test Assessment (PTA) aircraft were performed in three different NASA facilities. Wing and propfan nacelle static pressures, model forces and moments, and flow field at the pr... 展开
作者 | little, b. h. tomlin, k. h. | ||
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原报告号 | N8826360 | 总页数 | 157 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Prop-fan technology Wind tunnel tests Aircraft control Aircraft performance Aircraft stability Aircraft safety Flow distribution Scale models Static pressure Wind tunnel models |