본문 바로가기
PHAK

PHAK Chapter 6-13 Rudder

by ₯₺﷼₳ 2021. 8. 13.
반응형

Rudder

The rudder controls movement of the aircraft about its vertical axis. 

This motion is called yaw. 

 

Like the other primary control surfaces, the rudder is a movable surface hinged to a fixed surface in this case, to the vertical stabilizer or fin. 

 

The rudder is controlled by the left and right rudder pedals.

 

When the rudder is deflected into the airflow, a horizontal force is exerted in the opposite direction. 

 

By pushing the left pedal, the rudder moves left. 

 

This alters the airflow around the vertical stabilizer/rudder and creates a sideward lift that moves the tail to the right and yaws the nose of the airplane to the left. 

 

Rudder effectiveness increases with speed; therefore, large deflections at low speeds and small deflections at high speeds may be required to provide the desired reaction. 

 

In propeller-driven aircraft, any slipstream flowing over the rudder increases its effectiveness.

 

rudder
phak6_0152_rudder.mp3
0.23MB
phak6_0153.mp3
0.16MB
phak6_0154.mp3
0.29MB
phak6_0155.mp3
0.18MB
phak6_0156.mp3
0.22MB
phak6_0157.mp3
0.17MB
phak6_0158.mp3
0.28MB
phak6_0159.mp3
0.30MB
phak6_0160.mp3
0.22MB

반응형

'PHAK' 카테고리의 다른 글

PHAK Chapter 6-15 Secondary Flight Controls  (0) 2021.08.15
PHAK Chapter 6-14 V-Tail  (0) 2021.08.14
PHAK Chapter 6-12 Canard  (0) 2021.08.12
PHAK Chapter 6-11 Stabilator  (0) 2021.08.11
PHAK Chapter 6-10 T-Tail  (0) 2021.08.10

댓글