Theory of Flight
6.05 Lift and Drag
References:
Transport Canada Study and Reference Guide Glider Pilot
FTGU pages 91-98
Review
1. Name the 4 forces acting on an aircraft.
2. What are Newton’s 3 laws?
3. Is an aircraft considered to be in a state of
equilibrium when it is on the ground.
6.05 Lift & Drag
• MTPs:
– Bernoulli’s Principle- how lift is created
– Airfoil terms
– Angle of attack versus lift
– Angle of Incidence
– Types of airfoils
– Types of Drag
– Wingtip Vortices
– Streamlining
Bernoulli’s Principle
• Bernoulli’s Principle
– An increase in the speed of a fluid occurs
simultaneously with a decrease in pressure or
a decrease in the fluid's potential energy.
Bernoulli’s Principle
Speed Pressure
Speed Pressure
Bernoulli’s Principle
– Airfoils are shaped in a way to manipulate air
pressure based on Bernoulli’s principle.
– Air moves faster over the upper surface of the wing,
decreasing pressure (or increasing suction)
– Air moves slower over the lower surface of the wing
and creates a higher pressure, or pushing force.
Airfoil Terms
Terms related to airfoils
• Relative Airflow
• Angle of Attack
• Centre of Pressure
Relative Airflow
– The direction of the airflow with respect to the wing.
– It is created by the movement of the airplane as well as the
movement of air.
– Relative airflow is usually opposite to the flight path.
– Relative airflow itself is not related to lift
Angle of Attack
–The angle at which the airfoil meets the
relative airflow
Centre of Pressure
• Is the average of the pressure on an airfoil
– Sum of the distributed pressures on the airfoil acting
through a single straight line
• Moves forward on an airfoil as the angle of attack is
increased
Centre of Pressure
A of A versus Lift
• Now we know how we get lift but how much can we get?
• One factor affecting lift is Angle of Attack
– As the angle of attack increases, what happens to lift?
– BUT… As the angle of attack increases, what
happens to drag?
Lift Increases
Drag Increases
A of A versus Lift
Angle of
Attack
Lift/
Drag
Angle of Incidence
– The angle of incidence is the angle between
the mean aerodynamic chord of the wing and
the longitudinal axis of the aircraft
– The angle of incidence impacts forward
visibility, take-off and landing characteristics,
and drag in level flight
Types of Airfoils
• Airfoil
A two-dimensional surface designed to obtain a reaction from
the air through which it moves.
The shape of an airfoil will affect how air flows over the wing
Airfoil – 2D vs. Wing – 3D
Types of Airfoils
• What are some functions
of airfoils?
– Create lift
– Create thrust
– Attachment point for the
control surfaces (including
flaps, slots, slats, etc)
– House fuel tanks and
instrument components
–Stability
Confirmation Check
Confirmation
1. Label where the high pressure and low pressure are:
2. Fill in the blanks
__________________: The angle at which the airfoil meets the
relative airflow
__________________: airflow with respect to the wing
__________________:the average of the pressure on an airfoil
Confirmation
3. Lift acts 90o to the ________________.
4. Bernoulli’s principle states that:
An ____________ (increase/decrease) in the speed of a fluid occurs
simultaneously with a _____________________
(increase/decrease) in pressure or a _______________
(increase/decrease) in the fluid's potential energy
5. As lift increases, drag _______________.
Drag
– Is the resistance an airplane experiences in
moving forward through the air
Types of Drag
There are 2 main types of Drag:
1. Parasite Drag– This drag is further broken
down
– Form drag
– Skin Friction
2. Induced Drag
Parasite Drag
Drag of all those parts the airplane which
DO NOT contribute to lift
– This drag is hard to eliminate but it can be
minimized
• Form drag is caused by the shape of the
aircraft
– Landing gear
– Antennas
– Struts
– Wing tip fuel tanks
Parasite Drag
• Skin Friction
– The tendency of air
flowing over the body
to cling to its surface
– What causes it to
resist motion?
• Ice on the wings
• Dirt build up
Induced Drag
– Caused by those parts of an airplane which
are active in producing lift
– Cannot be eliminated
Lift Drag
Induced Drag
• Induced drag can be reduced with a high
aspect ratio
Wing Tip Vortices
• Over the top of the wing the
airflow goes inward
• Under the bottom of the wing
the airflow moves outward
Due to the
pressure changes
This creates a swirling motion off the wing tip called a vortex
Streamlining
• The less drag you have…
– Flying a glider: the further you can
fly
– Flying an airplane: the less fuel you
use
• Therefore streamlining is important
– A design device by which a body is
shaped to minimize drag
Confirmation
1. Fill in the diagram
2. Is it possible to eliminate induced drag? Why
or why not?
Wingtip Vortices

Lift and Drag.ppt

  • 1.
    Theory of Flight 6.05Lift and Drag References: Transport Canada Study and Reference Guide Glider Pilot FTGU pages 91-98
  • 2.
    Review 1. Name the4 forces acting on an aircraft. 2. What are Newton’s 3 laws? 3. Is an aircraft considered to be in a state of equilibrium when it is on the ground.
  • 3.
    6.05 Lift &Drag • MTPs: – Bernoulli’s Principle- how lift is created – Airfoil terms – Angle of attack versus lift – Angle of Incidence – Types of airfoils – Types of Drag – Wingtip Vortices – Streamlining
  • 4.
    Bernoulli’s Principle • Bernoulli’sPrinciple – An increase in the speed of a fluid occurs simultaneously with a decrease in pressure or a decrease in the fluid's potential energy.
  • 5.
  • 6.
    Bernoulli’s Principle – Airfoilsare shaped in a way to manipulate air pressure based on Bernoulli’s principle. – Air moves faster over the upper surface of the wing, decreasing pressure (or increasing suction) – Air moves slower over the lower surface of the wing and creates a higher pressure, or pushing force.
  • 7.
    Airfoil Terms Terms relatedto airfoils • Relative Airflow • Angle of Attack • Centre of Pressure
  • 8.
    Relative Airflow – Thedirection of the airflow with respect to the wing. – It is created by the movement of the airplane as well as the movement of air. – Relative airflow is usually opposite to the flight path. – Relative airflow itself is not related to lift
  • 9.
    Angle of Attack –Theangle at which the airfoil meets the relative airflow
  • 10.
    Centre of Pressure •Is the average of the pressure on an airfoil – Sum of the distributed pressures on the airfoil acting through a single straight line • Moves forward on an airfoil as the angle of attack is increased
  • 11.
  • 12.
    A of Aversus Lift • Now we know how we get lift but how much can we get? • One factor affecting lift is Angle of Attack – As the angle of attack increases, what happens to lift? – BUT… As the angle of attack increases, what happens to drag? Lift Increases Drag Increases
  • 13.
    A of Aversus Lift Angle of Attack Lift/ Drag
  • 14.
    Angle of Incidence –The angle of incidence is the angle between the mean aerodynamic chord of the wing and the longitudinal axis of the aircraft – The angle of incidence impacts forward visibility, take-off and landing characteristics, and drag in level flight
  • 15.
    Types of Airfoils •Airfoil A two-dimensional surface designed to obtain a reaction from the air through which it moves. The shape of an airfoil will affect how air flows over the wing Airfoil – 2D vs. Wing – 3D
  • 16.
    Types of Airfoils •What are some functions of airfoils? – Create lift – Create thrust – Attachment point for the control surfaces (including flaps, slots, slats, etc) – House fuel tanks and instrument components –Stability
  • 17.
  • 18.
    Confirmation 1. Label wherethe high pressure and low pressure are: 2. Fill in the blanks __________________: The angle at which the airfoil meets the relative airflow __________________: airflow with respect to the wing __________________:the average of the pressure on an airfoil
  • 19.
    Confirmation 3. Lift acts90o to the ________________. 4. Bernoulli’s principle states that: An ____________ (increase/decrease) in the speed of a fluid occurs simultaneously with a _____________________ (increase/decrease) in pressure or a _______________ (increase/decrease) in the fluid's potential energy 5. As lift increases, drag _______________.
  • 20.
    Drag – Is theresistance an airplane experiences in moving forward through the air
  • 21.
    Types of Drag Thereare 2 main types of Drag: 1. Parasite Drag– This drag is further broken down – Form drag – Skin Friction 2. Induced Drag
  • 22.
    Parasite Drag Drag ofall those parts the airplane which DO NOT contribute to lift – This drag is hard to eliminate but it can be minimized • Form drag is caused by the shape of the aircraft – Landing gear – Antennas – Struts – Wing tip fuel tanks
  • 23.
    Parasite Drag • SkinFriction – The tendency of air flowing over the body to cling to its surface – What causes it to resist motion? • Ice on the wings • Dirt build up
  • 24.
    Induced Drag – Causedby those parts of an airplane which are active in producing lift – Cannot be eliminated Lift Drag
  • 25.
    Induced Drag • Induceddrag can be reduced with a high aspect ratio
  • 26.
    Wing Tip Vortices •Over the top of the wing the airflow goes inward • Under the bottom of the wing the airflow moves outward Due to the pressure changes This creates a swirling motion off the wing tip called a vortex
  • 27.
    Streamlining • The lessdrag you have… – Flying a glider: the further you can fly – Flying an airplane: the less fuel you use • Therefore streamlining is important – A design device by which a body is shaped to minimize drag
  • 28.
    Confirmation 1. Fill inthe diagram 2. Is it possible to eliminate induced drag? Why or why not?
  • 29.