हमले-का-कोण हिंदी उपयोग और उदाहरण

""एयरोडाइनमिक माप के स्वचालित निगरानी और संचारण के लिए जटिल एयर डेटा कंप्यूटर (ADC) (कुल दबाव, स्थैतिक दबाव, हमले का कोण, पार्श्व-स्लिप).।

हमले-का-कोण इसके अंग्रेजी अर्थ का उदाहरण

The aircraft incorporates thrust vectoring and has adjustable leading–edge vortex controllers (LEVCONs) designed to control vortices generated by the leading edge root extensions, and can provide trim and improve high angle of attack behaviour, including a quick stall recovery if the thrust vectoring system fails.

This is because the effective angle of attack of the propeller blade decreases as airspeed increases.

To maintain the optimum effective angle of attack, the pitch must be increased.

Blade pitch angle is not the same as blade angle of attack.

As speed increases, blade pitch is increased to keep blade angle of attack constant.

A propeller blade's "lift", or its thrust, depends on the angle of attack combined with its speed.

In helicopters, pitch control changes the angle of incidence of the rotor blades, which in turn affects the blades' angle of attack.

Passive (stall-controlled) wind turbines rely on the fact that angle of attack increases with wind speed.

This is another use for twisted blades: the twist allows for a gradual stall as each portion of the blade has a different angle of attack and will stop at a different time.

Equivalently, the left wing's effective angle of attack is decreased due to the positive roll.

Though not as efficient as rudder mixing, aileron differential is very easy to implement on almost any airplane and offers the significant advantage of reducing the tendency for the wing to stall at the tip first by limiting the downward aileron deflection and its associated effective increase in angle of attack.

Those which require a high angle of attack on takeoff or landing are especially so.

The roll rate of a rudder roll is directly related to the angle of attack and mach number.