본문 바로가기
PHAK

PHAK Chapter 6-4 Ailerons

by ₯₺﷼₳ 2021. 8. 4.
반응형

Ailerons

Ailerons control roll about the longitudinal axis. 

 

The ailerons are attached to the outboard trailing edge of each wing and move in the opposite direction from each other. 

 

Ailerons are connected by cables, bellcranks, pulleys, and/or push-pull tubes to a control wheel or control stick.

 

Moving the control wheel, or control stick, to the right causes the right aileron to deflect upward and the left aileron to deflect downward. 

 

The upward deflection of the right aileron decreases the camber resulting in decreased lift on the right wing. 

 

The corresponding downward deflection of the left aileron increases the camber resulting in increased lift on the left wing. 

 

Thus, the increased lift on the left wing and the decreased lift on the right wing causes the aircraft to roll to the right. 

Ailerons
phak6_0037_ailerons.mp3
0.14MB
phak6_0038.mp3
0.14MB
phak6_0039.mp3
0.17MB
phak6_0040.mp3
0.17MB
phak6_0041.mp3
0.14MB
phak6_0042.mp3
0.16MB
phak6_0043.mp3
0.15MB

반응형

'PHAK' 카테고리의 다른 글

PHAK Chapter 6-6 Differential Ailerons  (0) 2021.08.06
PHAK Chapter 6-5 Adverse Yaw  (0) 2021.08.05
PHAK Chapter 6-3 Flight Control Systems  (0) 2021.08.03
PHAK Chapter 6-2 Introduction  (0) 2021.08.02
PHAK Chapter 6-1 Flight Controls  (0) 2021.08.01

댓글