1.The results show that the unstart boundary of supersonic inlets is mainly concerned with Mach number of freestream without considering the variation of angle of attack.
1.在不角变化的条件下,进气不起动边界主要与来数有关。
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1.Descend to and maintain FL 270. Do not exceed Mach number decimal 79.
384. 下降持高度270。不要超出马赫数点79。
2.Climb to and maintain FL310. Maintain Mach number decimal 81 or greater until BKM VOR.
383. 上持高度310。BKM VOR台前持马赫数点81或更大。
3.Radar service is terminated due technical failure. Maintain Mach number decimal 81 or less for separation.
426. 由于技术故障雷达服务终止。因间隔,持马赫数点81或更小。
4.Radar control is resumed, track direct to BKM VOR and increase speed to Mach number decimal 84.
428. 雷达管制恢复,直飞BKM VOR台,增速到马赫数点84。
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