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A preliminary study of a wake vortex encounter hazard boundary for a B737-100 airplane
| 题名： | A preliminary study of a wake vortex encounter hazard boundary for a B737-100 airplane |
| 作者： | Reimer, Heidi M.; Vicroy, Dan D. |
| 关键词： | boundary；counter；vortex；relim；study；lane；mina；simulation；forces；modified |
| 摘要： | A preliminary batch simulation study was conducted to define the wake decay required for a Boeing 737-100 airplane to safely encounter a Boeing 727 wake and land. The baseline six-degree-of-freedom B737 simulation was modified to include a wake model and the strip-theory calculation of the vortex-induced forces and moments. The guidance and control inputs for the airplane were provided by an autoland system. The wake strength and encounter altitude were varied to establish a safe encounter boundary. The wake was positioned such that the desired flight path traversed the core of the port Vortex. Various safe landing criteria were evaluated for defining a safe encounter boundary. A sensitivity study was also conducted to assess the effects of encounter model inaccuracies. |
| 报告类型： | 科技报告 |
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