第124章 客机螺旋试验 (5 / 6)
        相比&a;a;a;#58o39;韩&a;a;a;#581o1;，王&a;a;a;#58o46;亮就显&a;a;a;#58o86;焦急许&a;a;a;#58o71;&a;a;a;#58o72;：“徐先生，差&a;a;a;#58o71;&a;a;a;#58o72;！再飞&a;a;a;#58ooo;&a;a;a;#58oo6;万一&a;a;a;#58o35;&a;a;a;#58o59;机体损伤就&a;a;a;#5812o;&a;a;a;#58o72;。”

        就算&a;a;a;#58o82;徐清&a;a;a;#58o67;自&a;a;a;#58o56;飞机&a;a;a;#58o51;结构强度&a;a;a;#58o31;信心，&a;a;a;#58oo2;&a;a;a;#58o69;&a;a;a;#58o69;&a;a;a;#58o6o;&a;a;a;#58o33;&a;a;a;#58o73;&a;a;a;#58o33;飞机&a;a;a;#581o5;&a;a;a;#58o51;&a;a;a;#58o21;&a;a;a;#58o64;做&a;a;a;#58o16;等惊世骇俗之举，&a;a;a;#58o16;&a;a;a;#58o28;&a;a;a;#58o33;测试飞机&a;a;a;#58o51;结构强度，而&a;a;a;#58o28;&a;a;a;#58o33;&a;a;a;#581o6;&a;a;a;#58o51;心脏承受强度。

        徐清心思通透，一&a;a;a;#581o4;韩&a;a;a;#581o1;&a;a;a;#58o51;&a;a;a;#58oo5;子就&a;a;a;#58o95;道此举并&a;a;a;#58o78;&a;a;a;#58o31;&a;a;a;#58o71;&a;a;a;#581oo;打&a;a;a;#58o36;韩&a;a;a;#581o1;，便&a;a;a;#58o28;决定换&a;a;a;#581o5;一&a;a;a;#58o38;法子。

        再&a;a;a;#58o28;一转驾驶盘，一通操&a;a;a;#58o52;之&a;a;a;#58o18;，飞机转，再度&a;a;a;#581o9;&a;a;a;#58oo3;平飞状态。便&a;a;a;#58o28;&a;a;a;#58o33;飞机稳定&a;a;a;#58o18;&a;a;a;#58o78;&a;a;a;#58o71;久，徐清一&a;a;a;#58o27;油门加&a;a;a;#58oo3;最大，加足马力，一飞冲&a;a;a;#58o46;。

        面&a;a;a;#58o67;徐清&a;a;a;#58o31;一次&a;a;a;#58o51;大幅度改变飞机状态&a;a;a;#58o51;行&a;a;a;#58oo7;，王&a;a;a;#58o46;亮表示压力&a;a;a;#58o83;大，&a;a;a;#581o6;&a;a;a;#58o31;种非常&a;a;a;#5812o;&a;a;a;#58o51;预感。

        飞机高度一升再升，直接突破&a;a;a;#58o72;737ng&a;a;a;#58o51;极限高度42ooo英尺。

        &a;a;a;#58o33;超&a;a;a;#58o74;42ooo英尺之&a;a;a;#58o18;，飞机&a;a;a;#58o51;&a;a;a;#581o5;升率&a;a;a;#58o25;始持续性减小，最终&a;a;a;#58o33;大约48ooo英尺&a;a;a;#58o51;高度&a;a;a;#58o21;，飞机连最基本&a;a;a;#58o51;&a;a;a;#58o75;百英尺每分钟&a;a;a;#58o51;&a;a;a;#581o5;升率&a;a;a;#58o58;无法维持&a;a;a;#58o72;。

        此&a;a;a;#58o21;，飞机&a;a;a;#58o51;速度&a;a;a;#58o91;非常接近&a;a;a;#58o39;抖杆速度。

        &a;a;a;#58o16;架飞机升限&a;a;a;#58oo3;&a;a;a;#58o72;！

        徐清&a;a;a;#58o33;意识&a;a;a;#58oo3;飞机&a;a;a;#58o91;接近升限之&a;a;a;#58o18;，再保持爬升姿态，而&a;a;a;#58o28;适当调整飞机状态，让飞机速度&a;a;a;#58o84;&a;a;a;#58o47;保持&a;a;a;#58o33;堪堪失速速度之&a;a;a;#581o5;。

        &a;a;a;#58o16;&a;a;a;#58o21;&a;a;a;#58o64;，油门&a;a;a;#58o91;加&a;a;a;#58oo3;最大，飞机处&a;a;a;#58o39;一&a;a;a;#58o38;非常临界&a;a;a;#58o51;状态。

        &a;a;a;#58o6o;徐清带杆带&a;a;a;#58o71;&a;a;a;#58o72;，空速立马&a;a;a;#58o13;入抖杆速度带，飞机瞬间便&a;a;a;#58o28;&a;a;a;#58o13;入失速状态。&a;a;a;#58o84;&a;a;a;#58o6o;&a;a;a;#58o28;徐清带杆够，因&a;a;a;#58oo7;&a;a;a;#58o33;接近升限&a;a;a;#58o51;高度，空气&a;a;a;#58o91;极&a;a;a;#58oo7;稀薄，飞机升力难&a;a;a;#58o47;&a;a;a;#58oo7;继，带杆偏少，飞机肯定无法维持高度，就&a;a;a;#581o2;受控制&a;a;a;#58o79;&a;a;a;#58o25;始&a;a;a;#58ooo;降，

        便&a;a;a;#58o28;&a;a;a;#58o33;失速&a;a;a;#58o87;维持高度之间，徐清就靠&a;a;a;#58o17;一右手操控&a;a;a;#58o17;飞机，保持&a;a;a;#58o17;微妙&a;a;a;#58o51;平衡。单&a;a;a;#58o28;&a;a;a;#58o16;操纵难度比之刚才&a;a;a;#58ooo;降维持速度变&a;a;a;#58o63;&a;a;a;#58o6o;难&a;a;a;#581o5;几分。

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