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 ... 展开
作者 | Reimer, Heidi M. Vicroy, Dan D. | ||
---|---|---|---|
原报告号 | NASA-TM-110223 | 总页数 | 18 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | BOEING 737 AIRCRAFT VORTICES AIRCRAFT WAKES FLIGHT PATHS SPACING AIRCRAFT HAZARDS FLIGHT HAZARDS AIRCRAFT GUIDANCE FLIGHT SIMULATION AIR NAVIGATION CLEARANCES |