摘要: Flight tests were made to demonstrate the particularity of employing fixed tabs in conjunction with a suitably designed differential linkage to reduce the force required to operate ailerons. The tests showed the system to be pract... 展开
作者 | Soule, H A Hootman, James A | ||
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原报告号 | naca-tn-653 | 总页数 | 25 |
报告类别/文献类型 | NASA / NTIS科技报告 |