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Principles of Flight

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Principles of Flight Spitfire Chapter 1 Weight and Lift How is an aircraft, which is much heavier than the air it flies in, supported by the air? – PowerPoint PPT presentation

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Title: Principles of Flight


1
Principles of Flight
Spitfire
2
Chapter 1 Weight and Lift
  • How is an aircraft, which is much heavier than
    the air it flies in, supported by the air?

C130
3
  • Sir Isaac Newton formulated laws to explain the
    movement of objects.
  • Newtons Third Law states that to every action
    there is an equal and opposite reaction.
  • For example Imagine a car weighing 10,000N
    parked on the road. The cars weight presses down
    on the road with a force of 10,000N and from
    Newtons third law the road must be supporting
    the car and pushing up with an equal and opposite
    force of 10,000N.

4
  • How does this apply to an aircraft flying?
  • How can an aircraft which might weigh many tonnes
    be supported by such a flimsy substance such as
    air?
  • One clue is that an aircraft can only stay
    airborne as long as it is moving. (except a
    Harrier of course!)

5
Air is a substance
  • Moving air can exert forces on objects e.g. in
    hurricanes
  • The greater the speed, the greater the force it
    exerts.
  • Conclusion Air is undoubtedly a very real
    substance, invisible as it is!

6
Moving objects through air
  • Is there a force if an object is moving through
    stationary air?
  • Imagine cycling along a flat road on a perfectly
    calm day. As your speed increases, you will
    begin to feel the air on your face. The faster
    you pedal the greater the force of this apparent
    wind.
  • Whether you have air moving past a stationary
    object or an object moving through stationary
    air, similar forces are experienced.

7
  • Every object has weight.
  • The weight of an aircraft must be supported or
    lifted by a force.
  • How is this lifting force to be given to an
    aircraft?

8
Try this Hold two sheets of paper with the edges
vertical and about finger width apart. What will
happen if you blow between the two pieces of
paper?
9
What causes this to happen?
  • Wind Tunnel Test
  • The air goes in at point A, passes the
    constriction at point B, and comes out at point
    C.
  • What are the speeds and pressures at points A, B
    and C?

10
Bernoullis Principle
  • The same amount of air enters B as is leaving,
    therefore the speed of air at B must increase to
    pass through the narrowest part of the tube.
  • The increased speed of the air at B, creates a
    streamlined flow (non-turbulent) which exerts
    less pressure on the tube.
  • Conclusion Air moving a increased speeds exerts
    less pressure or creates an area of lower
    pressure.

11
  • Can you now explain why the two pieces of paper
    move together when you blow air between them?

12
Proving the theory
  • Try this Hold a half sheet of A4 (halved
    lengthways) such that the end between you fingers
    is horizontal, but allow the rest of the paper to
    curve downwards under its own weight. Then blow
    along the curved top of the paper only.
  • What happens?

13
  • Observation The paper rises in line with the
    air flow.
  • By speeding up the air over top you have reduced
    the pressure above the paper, so the air pressure
    under the paper pushes it up.
  • What happens when you blow harder?
  • The harder you blow the more it rises.

14
Lift
  • The top surface of an aircrafts wing is shaped
    such that air which flows between it and the
    undisturbed air a little way above the wing is,
    in effect, being forced through a constrictions.
  • The air flows over the wing at an increased
    speed-and therefore at a reduced
    pressure-compared with the surrounding atmosphere

15
  • The resulting pressure difference between the air
    above and below the wing tends to lift it up.
  • This is not the only thing that contributes to
    lift. In real life, the airflow rarely approaches
    a wing as shown above.
  • In most flight conditions, the wing is inclined
    to the airflow at a slight positive angle so that
    it deflects some of the airflow downwards.
  • This results in an upward force, though not
    normally as much as the lift generated by the top
    surface of the wing

16
Distribution of lift
  • There are pressure forces acting all over the
    wing- and there can be lift forces all over the
    wing
  • The length of each arrow indicates the amount of
    lift at that point on the wings surface.

Pressure patterns near A wing
17
  • Note that
  • Lift is not distributed evenly around the wing
  • The top surface generates more lift than the
    bottom surface (sometimes as much as 80 of the
    total!)
  • The greatest amount of lift on the top surface
    occurs where the surface is curved the most.
  • The greatest effect, on both top and bottom
    surfaces, is nearer the front edge of the wing
    than the rear (1/3 of the way from the front)
  • All lift forces act at 90 to the direction of
    the airflow.

18
Centre of Pressure
  • We normally add all the forces together and
    represent them by a single straight line.
  • This force is drawn from the point at which all
    the forces balance.
  • This is the point which all the lift can be said
    to act and it is called the centre of pressure.

19
How Lift Varies
  • Several factors affect the amount of lift
    produced by a wing
  • A) Air speed greater airspeed creates greater
    lift (doubling the airspeed, quadruples the
    lift!)

20
  • B) Angle of attack- This is the angle between the
    chord line of the wing and the oncoming air. A
    pilot can alter this by altering the pitch
    attitude of the aircraft- by easing forward or
    pulling back on the controls. The lift will
    increase until the angle reaches about 15.
    Beyond this point, the lift rapidly decreases and
    the wing has stalled

21
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22
  • C) Air Density If air becomes thinner or less
    dense ( at increased height temperature or
    humidity), the amount of lift is reduced. To
    calculate the take off run the pilot would use
    tables which allow for engine performance,
    weight, wind speed and direction, and of course
    the air temperature, humidity and density.

23
  • D) Wing shape and area- The shape of the wing
    section and the plan area of the wing are
    calculated by the aircraft designer to suit the
    aircrafts role and required performance.
  • A high-lift section would be used where good lift
    at low speeds is all-important

24
  • General Purpose section would suit a moderately
    fast aircraft, not intended to approach the speed
    of sound.
  • More lift for any given wing section and
    airspeed can be found by increasing the plan area
    of the wing- that is, by making the wing bigger.

25
  • Unfortunately a bigger wing is heavier and also
    more resistant to rapid manoeuvres- not
    acceptable for air combat aircraft.
  • Hinged flaps fitted to most light aircraft have
    the effect of increasing the camber of the wing
    when they are lowered.
  • More advanced Fowler flaps slide backwards to
    increase the wing area, as well as hinging
    downwards

26
Lift and Weight in Straight and Level Flight
  • The lift force equals the force of gravity acting
    on the aircraft (its weight)
  • If the lift is greater than the weight, an
    aircraft will climb
  • If the weight is more than the lift, it will
    descend.

27
Questions
28
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