摘要: Many conceptual designs for advanced short-takeoff, vertical landing (ASTOVL)aircraft need exhaust nozzles that can vector the jet to provide forces and moments for controlling the aircraft's movement or attitude in flight near th... 展开
作者 | Mcardle, J. G. Esker, B. S. | ||
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原报告号 | N9327131 | 总页数 | 34 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Exhaust nozzles Nozzle design Nozzle flow Parallel flow V/stol aircraft Performance tests Aircraft design Footprints Gas jets Powered lift aircraft Vertical landing |