Angle of attack sensing system

攻角感测系统

Angle of attack at minimum drag

最小阻力攻角

Angle of attack at maximum lift

最大升力攻角

Angle of attack decreases with increasing speed.

攻角随增加的速度。

The existence of angle of attack reduces the inlet performance.

攻角的存在也在一定程度上降低了进气道性能.

This occurs at one angle of attack for the same wing loading of a paraglider.

这种情形会发生于飞行伞的翼负载相当于攻角时。

The influence of velocity of water-exit and angle of attack to cavitation of parts of missile was analyzed.

分析了出水速度及攻角对弹体各部件空泡的影响。

The steady laminar flow field of a hypersonic sharp cone boundary layer with zero angle of attack was computed.

先计算出高超音速零攻角尖锥边界层的定常层流流场。

Effects of flap deflection angle, angle of attack, Mach number and unit Reynolds number are discussed.

讨论了翼偏角、攻角、马赫数和单位雷诺数对热流与压力特性的影响。

The static aerodynamic characteristics for slender bodies at large angle of attack was analyzed.

研究分析了细长旋成体弹身类型气动外形的大攻角范围气动特性.