摘要: This report contains the flight-test results of the lateral and directional-stability and control phase (including tests with wing-tip tanks) of a general flying-qualities investigation of the Lockheed P-80A airplane (Army No. 44-... 展开
作者 | Anderson, S. B. Cooper, G. E. | ||
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原报告号 | N20030063229 | 总页数 | 55 |
主办者 | National Aeronautics and Space Administration | ||
报告分类号 | [51C - Aircraft51F - Test Facilities & Equipment] | ||
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Directional stability Flight characteristics Flight tests Control stability Lateral stability Aircraft design Mach number Rudders Static stability Ailerons Low altitude Airspeed Wing tips Wing tanks |