1. Basic Aeronautics
Know the principles of basic aeronautics. 1. Describe the effects of angle of attack. 2. Identify the four forces of flight.
Lesson Objective: Know the principles of basic aeronautics.
Samples of Behavior/Main Points
1. Describe the theory of flight.
2. Describe airfoil design.
3. Describe the effects of relative wind.
4. Describe the effects of angle of attack.
5. Identify the four forces of lift.

2. Review Newton’s Three Laws:
A body at rest tends to remain at rest, and a body in motion tends to stay in motion, unless an outside force acts on the body.
Force = Mass x Acceleration.
For every action there is an equal and opposite reaction.

3. The Four Forces of Flight
Increase velocity of air around an airfoil shape = increases the relative wind as it flows above and below the surface of the airplane wing.
The Four Forces of Flight
Lift
According to Bernoulli’s Principle, there is increase in the velocity of air as the air flows around an airfoil shape.
Because the camber of the upper wing surface is greater than that of the lower surface, air flowing above the wing will be increased more than air flowing beneath the wing.
The Bernoulli’s Principle also states that an increase in the velocity of a fluid, such as air, results in a decrease of pressure within that fluid. As a result, the reduction in air pressure above the wing will be greater than the pressure reduction along the lower wing surface.

4. Angle of Attack
Formed by the cord of the airfoil and the direction of the relative wind or between the chord line and the flight path.
Is not constant during a flight. It changes as the pilot changes the attitude of the aircraft.
Angle of Attack
The angle of attack is formed by the chord of the airfoil and the direction of the relative wind or between the chord line and the flight path.
The angle of attack is not constant during a flight. It changes as the pilot changes the attitude of the aircraft.
The angle of attack is one of the factors that determines the aircraft’s rate of speed through the air.

5. The Four Forces of Flight
Angle of Attack
Angle of Attack Again
Changing the angle of attack can change the amount of lift generated as the airfoil moves through the air.
Airflow over an airfoil is normally smooth with no turbulence. In the case of an airfoil with a flat or approximately flat undersurface and when the lower surface is parallel to the relative wind, there is no impact pressure on the lower surface.
The whole lift force comes from reduced pressure along the upper surface (pressure-differential lift).
When the wing is tipped up so that the lower surface makes an angle of 5 with the relative wind, the impact pressure on the undersurface contributes about 25 percent of the total lift.
When it is tipped up to 10, the impact pressure on the lower surface produces about 30 percent of the total lift.
A small force acts on each tiny portion of the wing. This force is different in magnitude (size) and direction from the force acting on other small areas of the surface farther forward or rearward.

6. The Four Forces of Flight
Angle of Attack
The angle at which lift stops increasing and begins to decrease is called the burble point.
The angle at which lift stops increasing and begins to decrease is called the burble point.
This angle may also be called the stalling angle or the angle of maximum lift.
When the angle of attack is increased beyond the burble point, the resultant decreases in magnitude and its angle back from the vertical becomes bigger.
At the various angles just described, the direction of the resultant has had an upward and backward direction.
As the angle of attack is increased, more and more lift is generated. This increase in amount of lift continues up to a certain angle of attack (the burble point, mentioned previously) which depends on the type of wing design.
Most aircraft wings have a burble point of somewhere between 15 and 20°, but this is built into the aircraft.
When the air no longer flows smoothly over the top surface of the airfoil it is called burbling. When burbling is taking place on a surface, there can be no decrease in pressure below the atmospheric pressure.

7. The Four Forces of Flight
Angle of Attack
The point at which the amount of lift generated is no longer sufficient to support the aircraft in air is called the stalling point.
The point at which the amount of lift generated is no longer sufficient to support the aircraft in air is called the stalling point, and the maneuver in which the pilot does this is called the stall.

8. The Four Forces of Flight
Lift can be increased in two ways
Increasing the forward speed of the airplane.
Increasing the angle of attack.
The pilot can increase the forward speed of the aircraft by applying more power.
Lift can be increased in two ways: by increasing the forward speed of the airplane or by increasing the angle of attack.
The pilot can increase the forward speed of the aircraft by applying more power. This increases the speed of the relative wind over the airfoil.

9. The Four Forces of Flight
Lift Variables
Atmosphere
Airfoil Shape
Wing Area
Weight
Thrust and Drag
Lift Variables
The pilot must have some way to control the amount of lift the airfoils generate.
If the pilot didn’t, the aircraft would either constantly stall or climb.
There are variables acting on the amount of lift generated.
Angle of attack
Velocity of relative wind (speed of the aircraft)
Air density
Airfoil shape
Wing area
Airfoil platforms
High-lift devices.

10. The Four Forces of Flight
Air Density and Lift
Lift varies directly with air density. At 18,000 feet air density is about half that at sea level. At that altitude an aircraft will need to fly faster maintain altitude.
Air Density and Lift
Air density is another variable factor that can influence lift. The first thing to note is that lift varies directly with density.
For instance, at 18,000 feet, where the density is about half that at sea level, an aircraft will need to travel times as fast as it would at sea level to maintain altitude. The number is the square root of 2.
If something reduces the lift by half, it has to increase the speed so that the square of the new velocity is twice the square of the original velocity.
Lift Variables
Atmosphere
Airfoil Shape
Wing Area
Weight
Thrust and Drag

11. The Four Forces of Flight
Airfoil Shape
It is extremely important to preserve the characteristic curve that the designers built into the airfoil.
Dents, mud, and ice are three common things that can spoil the built-in shape of the airfoil and interfere with the performance of the entire aircraft.
Airfoil Shape as a Variable
Up to a certain point, the greater the camber, the greater the lift.
It becomes extremely important once an airfoil has been designed, to preserve the characteristic curve that the designers build into the airfoil.
Dents, mud, and ice are three common things that can spoil the built-in shape of the airfoil and interfere with the performance of the entire aircraft.
Lift Variables
Atmosphere
Airfoil Shape
Wing Area
Weight
Thrust and Drag

12. The Four Forces of Flight
Wing Area and Lift
The greater the surface area of the wing, the greater the amount of lift that will be generated.
Gliders and sailplanes are very good examples of how a large wing surface generates lift.
Wing Area and Lift
If the pressure differential is only 2½ ounces per square inch (a very small amount of differential pressure), this will produce a lifting force of more than 20 pounds per square foot (144 square inches/square foot x 2½-ounces/square inch).
The greater the surface area of the wing, the greater the amount of lift that will be generated, within practical limitations if the proportions of the wing and the airfoil section stay the same.
Gliders or sailplanes are very good examples of how a large wing surface generates lift.
Lighter, stronger, materials are being developed, so that today’s aircraft can be built to withstand tremendous strains and yet not be heavy.
Lift Variables
Atmosphere
Airfoil Shape
Wing Area
Weight
Thrust and Drag

13. The Four Forces of Flight
Weight
There is a point where lift can no longer overcome weight.
The airplane must be constructed of the lightest weight materials that can be used.
The weight of whatever the airplane carries also receives very careful consideration.
There is another situation where lift can no longer overcome weight. This limit is called the aircraft's ceiling. At its ceiling, the aircraft's power plant is producing all possible power, and the airfoils are producing all possible lift just to equal the force of the aircraft's weight.
The atmosphere becomes less and less dense as altitude increases. The aircraft's ceiling is that point in the atmosphere where the air is too thin to allow further increase in lift.
The airplane must be constructed of the lightest weight materials that can be used. Most airplanes today are built of metal. Aluminum alloy is used extensively in aircraft construction because of its strength and light weight.
The weight of whatever the airplane carries also receives very careful consideration. Each airplane has a total weight limitation called the maximum allowable gross weight above which the airplane is unsafe for flight.
Lift Variables
Atmosphere
Airfoil Shape
Wing Area
Weight
Thrust and Drag

14. The Four Forces of Flight
Weight
Where the weight, or useful load, is placed in the airplane is another factor that has a pronounced effect on how well an airplane will fly.
The pilot has to subtract the empty weight from the maximum allowable gross weight to find out how many pounds may be loaded into the airplane. This is the useful load.
Where the weight, or useful load, is placed in the airplane is another factor that has an effect on how well the airplane will fly.
This is because the center of gravity of the airplane must be within certain limits prescribed by the manufacturer.
These limits are based on where the center of lift (CL) of the particular design happens to be.
If placement of the useful load moves the center of gravity too far forward or too far aft of the CL, the airplane will be difficult, if not impossible, to control while in flight
Lift Variables
Atmosphere
Airfoil Shape
Wing Area
Weight
Thrust and Drag

15. The Four Forces of Flight
Thrust and Drag
Thrust is the force that propels the aircraft forward.
An airplane cannot gain altitude or maintain straight and level flight unless its engine is producing enough thrust.
Without the needed thrust, weight has more influence than lift and pulls the airplane toward the ground.
Thrust and Drag
Thrust is the force that propels the aircraft forward. Thrust for aircraft is obtained from different types of engines.
An airplane cannot gain altitude or maintain straight and level flight unless its engine is producing enough thrust to propel (pull or push) the airfoils fast enough to produce the needed amount of lift.
Without this thrust, the airplane will continue to fly. It will not “drop out of the sky” as many people think, but its flight becomes a gradual descent toward the ground.
Without the needed thrust, weight has more influence than lift and pulls the airplane toward the ground. Helping the force of weight is drag.
Lift Variables
Atmosphere
Airfoil Shape
Wing Area
Weight
Thrust and Drag

16. The Four Forces of Flight
Thrust and Drag
Drag is present all the time and can be defined as the force that opposes thrust.
The friction of air particles rubbing against all parts of the airplane causes part of the total drag.
The shape of something may create low-pressure areas and turbulence that retard the forward movement of the aircraft.
Drag is present at all times and can be defined as the force that opposes thrust. Better yet, drag is the force that opposes all motion through the atmosphere and is parallel to the direction of the relative wind.
The friction of air particles rubbing against all parts of the airplane causes part of the total drag. In fact, airspeed can be increased several miles per hour if the surfaces of the airplane are kept highly polished.
The shape of something may create low-pressure areas and turbulence that retard the forward movement of the aircraft. Streamlining the aircraft will reduce form drag.
Parts of an aircraft that do not lend to streamlining are enclosed in covers, called fairings (or cowling for an engine), that have a streamlined shape.
Lift Variables
Atmosphere
Airfoil Shape
Wing Area
Weight
Thrust and Drag

17. Summary 1. Angle of Attack 2. The Four Forces of Flight
In this lesson we discussed:
1. Theory of Flight
2. Airfoils and Flight
3. Relative Wind
4. Angle of Attack
5. The Four Forces of Flight