Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
36 Cards in this Set
- Front
- Back
What is the definition of a stall?
|
Condition in flight where an increase in AOA results in a decrease in C*L
|
|
Laminar Flow
|
Produces Lift
|
|
Turbulent Flow
|
Does not produce lift
|
|
Define Boundary Layer
|
Thin layer of air near the surface of an airfoil where air is affected by the air foil
|
|
What area on a wing surface does air have the highest kinetic energy and the least amount of pressure above which the most lift is created?
|
Max point of thickness
|
|
what is produced in a boundary layer separation?
|
Turbulent Flow
|
|
What causes a turbulent Flow?
|
Adverse Pressure Gradient
|
|
What is the cause of an adverse pressure gradient?
|
Low Pressure behind the max point of thickness
|
|
what controls an adverse pressure gradient?
|
Kinetic energy of the relative wind
|
|
What is the impact of a High AOA on the boundary layer?
|
1. kinetic energy decreases 2. Adverse pressure gradient increases 3. Boundary layer separation moves forward on the airfoil
|
|
define Boundary Layer separation
|
Point in streamline where airflow no longer adheres to the airfoil
|
|
what is the impact of boundary layer separation?
|
The Airfoil no longer produces lift sufficient to overcome weight
|
|
What causes Boundary layer separation?
|
High AOA
|
|
Where does the stall region on the boundary layer separation start?
|
C*LMAX
|
|
What is constant for every airfoil and is measured in arbitrary units?
|
Stall AOA
|
|
Is Stall airspeed the same for all airfoils?
|
No, it varies based on the airspeed and AOA
|
|
What are the two key differences between Power-off and Power-on stalls?
|
1.Vertical Component of thrust 2. Propeller Acceleration factor
|
|
Define Power-off stalls
|
Power setting: IDLE, High Stall Speed, Stall warning near stall, Right turning tendancy
|
|
Define Power-on stalls
|
Power setting: above IDLE, Lower Stall Speed, Stall warning above stall, Left turning tendancy
|
|
Which stall has a RIGHT turning tendency?
|
Power-off
|
|
Which stall has a LEFT turning tendency?
|
Power-on
|
|
What factors affect stall speed?
|
1. Gross weight 2. Altitude (air density) 3. Load Factor
|
|
What happens to stall speed of an aircraft when the weight increases?
|
Stall speed also increases
|
|
What happens to stall airspeed when altitude increases?
|
True stall speed increases but indicated stall speed stays the same
|
|
Increased G-loading is equivalent to increasing the weight
|
TRUE
|
|
What must increase with increased bank angle?
|
G-load, and stall speed
|
|
How many Gs are required to maintain level flight in a 60 degree bank?
|
2Gs
|
|
How is Boundary Layer controlled?
|
deflection of kinetic energy airflow from the bottom of an airfoil to the top of an airfoil
|
|
What is the most common Boundary layer control device?
|
Leading Edge Slats or Slats
|
|
What are the two benefits of Boundary Layer Control?
|
1. Increased maneuvering capabilities 2. Decreased landing speed and distance.
|
|
In what order will you lose control surfaces in a stall?
|
1. ailerons 2. Elevator 3. Rudder
|
|
T-6A stall AOA
|
18 units
|
|
What is the cause of buffet in the stick during a stall?
|
Turbulent airflow over the empannage
|
|
When does the buffet occur in the T-6A for power-on and power-off stalls?
|
Power-on - little natural effect of buffet before stall. Power-off - Approx 3 Knots before stall.
|
|
What are the two indications in the T-6A of a stall?
|
1. AOA gauge reading at 18 units 2. Stick Shaker
|
|
When does the stick shaker activate in the T-6A?
|
1. Approx. 15.5 AOA 2. minimum 5 knots before stall
|