User Guide
Learning To Fly with Rod Machado
71
7
Angle of Attack
The angle between the
wing and the wind that
blows on it is called the
angle of attack, as shown in
Figure 5.
In cruise flight at 110 knots, the
angle of attack is relatively small,
resulting in a near-level pitch
attitude, as shown in Figure 6A.
When we slowed the airplane
down, the autopilot, in order to hold
altitude, increased the angle of
attack by raising the airplane’s
pitch attitude, as shown in Figure
6B.
In cruise flight, the wing’s
engineered shape curves the air
enough to provide the necessary lift for flight. This allows us to fly at a small angle of attack. When the
airspeed decreases, however, the wing’s engineered shape can’t bend or curve the air sufficiently to
produce adequate lift. Therefore, we needed to artificially bend the air flowing over the wing by
making the wing attack the air at a larger angle. A larger angle of attack imparts a larger bend or
curve to the wind, causing the wind’s speed to increase as it flows aft. This results in an increase in
lift even though the airplane is flying at a slower airspeed.
At this point you’re probably thinking, “Hmmm, instead of learning to fly, maybe I should try
something simpler, like neurosurgery.” Don’t fret. You now have enough information to understand
the process of slow flight. Do you see the relationship between angle of attack and airspeed?
As the airspeed decreases, you must increase the angle of attack to maintain altitude. In other words,
to maintain level flight, you must increase the airplane’s pitch attitude by applying rearward pressure
on the joystick. At higher airspeeds, the wing’s engineered shape produces sufficient lift for level
flight at a near-level pitch attitude. Now you know why commercial airliners need large nose-up pitch
attitudes on liftoff since their takeoff speeds are so low. Once the jetliner accelerates to its cruise
speed, it flies along at a lower pitch attitude. Let’s put our knowledge to practice.
Figure 6
Figure 5
AIRPLANE’S MOTION
RELATIVE MOTION
ANGLE OF
ATTACK
A
B










