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本文在全包线范围内,计算分析了某战斗机基准飞行状态为ny_0=0～0.8ny_(max)情况下的滚转性能,并用美国军用规范《MIL-F-8785C》的相应条款对比作了品质检查,最后给出了几点结论和看法。
In this paper, the rollover performance of a fighter under the condition of ny_0 = 0 ~ 0.8ny max is calculated and analyzed in the range of all-enveloping line and compared with the corresponding provisions of MIL-F-8785C Quality inspection, and finally gives a few conclusions and opinions.