SPC - Student Pilot Certificate Basic Aerodynamics Principles Questions and Answers

Question 1

Which of the following describes the relationship between airspeed, angle of attack (AOA), and lift in straight-and-level flight?

Accepted Answer

To maintain constant lift, if airspeed decreases, the angle of attack must increase.

Answer

In straight-and-level flight, lift must equal weight. Lift is generated by the movement of air over the wings. If the aircraft slows down (airspeed decreases), the wing must be presented to the oncoming air at a higher angle of attack to generate the same amount of lift required to counteract weight.

Question 2

What are the four fundamental forces acting on an airplane in flight?

Accepted Answer

Lift, Weight, Thrust, and Drag

Answer

The four fundamental forces of flight are lift (the upward force created by the wings), weight (the downward force of gravity), thrust (the forward force from the engine/propeller), and drag (the rearward force of air resistance).

Question 3

A pilot is on final approach for landing and extends the flaps. What is the primary aerodynamic reason for using flaps during this phase of flight?

Accepted Answer

To allow the aircraft to fly at a slower airspeed while maintaining sufficient lift.

Answer

Extending flaps increases the wing's camber and, in some cases, its surface area. This allows the wing to produce the required lift at a lower airspeed, enabling a slower and steeper approach for landing.

Question 4

According to Bernoulli's Principle, how is lift generated by an airfoil?

Accepted Answer

By creating an area of lower pressure above the wing and higher pressure below it.

Answer

Bernoulli's Principle states that as the velocity of a fluid (like air) increases, its pressure decreases. The curved shape of an airfoil forces the air flowing over the top to travel a longer distance, and thus faster, than the air flowing underneath. This creates lower pressure above the wing and higher pressure below, resulting in an upward force called lift.

Question 5

The 'critical angle of attack' is the point at which...

Accepted Answer

lift is at its maximum and the wing will stall if the angle is increased further.

Answer

The critical angle of attack is the angle at which the wing produces its maximum lift coefficient. If the angle of attack is increased beyond this point, the airflow over the upper surface of the wing will separate, causing a rapid decrease in lift and an increase in drag. This condition is known as a stall.

(SPC) Student Pilot Certificate Practice Test

(SPC) Student Pilot Certificate Practice Test

SPC - Student Pilot Certificate Basic Aerodynamics Principles Questions and Answers