25.11.2014 Views

Heads-Up Display Modes 35 - Metaboli

Heads-Up Display Modes 35 - Metaboli

Heads-Up Display Modes 35 - Metaboli

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

Ground School 109<br />

therefore causing the aircraft to slow down. Slowing down subsequently reduces<br />

lift and drag, allowing the aircraft to accelerate again.<br />

hA stall can occur at any altitude, airspeed, or flight attitude.<br />

Increasing AOA eventually disrupts the airflow over the wing. This is called stalling<br />

the aircraft. During a stall, the reduced airflow over the wing severely decreases<br />

the amount of lift generated. A stall can occur at any altitude, airspeed, or flight<br />

attitude simply by increasing the AOA too much. A stall can have disastrous<br />

consequences during a dogfight, as explained below in the “Lift, Turn Rate, and<br />

Turn Radius” section. Learn to avoid stalling during a dogfight.<br />

If the aircraft sideslips during a stall, the aircraft is likely to depart controlled flight.<br />

In most cases, this “departure” results in a spin, but some aircraft are prone to<br />

other types of rocking, pitching, and tumbling. During a departure, the pilot has no<br />

control over the aircraft and must focus on regaining controlled flight. To recover<br />

from a spin, reduce the throttle and apply rudder opposite to the direction of the<br />

spin. In most cases, pushing the control stick forward helps, also. Hold these<br />

flight controls until the aircraft stops spinning and responds to control inputs. It is<br />

common to lose several thousand feet of altitude during a spin.<br />

hTo recover from a spin: Reduce throttle, apply rudder opposite to the<br />

direction of the spin. It often helps to push the control stick forward,<br />

also. Hold these controls until the aircraft stops spinning.<br />

8.004 Lift, Turn Rate, and Turn Radius<br />

The lift vector (the direction of the g-load generated by the wings) is perpendicular<br />

to the wings. As long as lift equals gravity, the aircraft maintains a steady altitude.<br />

Banking the aircraft reduces the amount of lift directly opposing gravity.<br />

How Bank Angle Affects G-Load<br />

Aircraft performance is generally described in terms of turn rate and turn radius,<br />

both of which are dependent upon the aircraft’s speed and the amount of lift, or g-<br />

load, being produced. Turn rate measures the speed at which the nose is moving<br />

around the circle, typically measured in degrees per second. A high turn rate<br />

means the aircraft could complete a 360° turn very quickly. Turn radius, as the<br />

name implies, measures the size of the aircraft’s turn. The ideal fighter couples a<br />

low turn radius with a high turn rate.

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!