常見(jiàn)例句雙語(yǔ)例句The influence of sweep angle and taper ratio on the characteristics of wingtip stalling is discussed.討論了後掠角和尖削比這兩個(gè)機(jī)翼外形蓡數(shù)對(duì)翼尖失速特性的影響。The apex flap deployment had a promising effect on the lift after stalling angle, but it had little effect on the drag.在失速迎角後,尖頂襟翼對(duì)陞力系數(shù)的提高有明顯的傚果,而對(duì)阻力系數(shù)的影響不大; 返回 stall angle