摘要: This report presents the results of flight tests made on five different lateral control devices that appeared adaptable to wings fitted with full span flaps: controllable auxiliary airfoils (airfoils mounted above and forward of t... 展开
作者 | Soule, H A Mcavoy, W H | ||
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原报告号 | NACA-TR-517 | 总页数 | 11 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | MONOPLANES AIRCRAFT CONTROL LATERAL CONTROL CONTROL SURFACES AILERONS WING FLAPS FLIGHT TESTS LIFT AERODYNAMIC COEFFICIENTS CHORDS (GEOMETRY) SPLIT FLAPS RETRACTABLE EQUIPMENT POSITION (LOCATION) |