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Aeromodelling event

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By making a good aerofoil. By optimizing the angle of attack to have good lift to drag ratios. Types of aerofoil. Angle of Attack(aoa) Relation between aoa & lift ... – PowerPoint PPT presentation

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Title: Aeromodelling event


1
Aeromodelling event
The Wright Design
2
  • Model airplanes are sized down models of an
    aircraft
  • The calculations are easy and the importance is
    given to building of the plane

3
Basic Aerodynamics
4
Forces acting on a plane
5
Lift
  • Its the upward force acting on the plane due to
    the air flow over the wings
  • It is determined by the design of the wing and
    the wind nature as
  • L1/2?V2ACL
  • CL is the lift coefficient
  • V is flight speed , A is wing area
  • ? is density of air

6
Thrust
  • Its the force provided by the engine of the
    plane
  • Mainly two type of thrust generators are used
  • IC Engines
  • Electric Motors
  • We will be seeing about electric motors here

7
Weight
  • This is the weight of the plane along with its
    payload and motors
  • This should be minimized as much as possible by
    proper design

8
Drag
  • This is the force that opposes the motion of the
    plane and is basically the air friction
  • This too can be reduced by having proper
    construction of the surfaces of the plane

9
Wing Aspects
10
Wings and Aerofoil
  • The lift generation is decided by the shape of
    the wings and the aerofoil
  • The lifting force is provided by the difference
    in the pressure of air flowing below and above
    the wing and is governed by Bernoullis principle

11
How do you design a good wing?
  • By proper calculation of the wingspan , wing
    loading and aspect ratios
  • By making a good aerofoil
  • By optimizing the angle of attack to have good
    lift to drag ratios

12
Types of aerofoil
13
Angle of Attack(aoa)
This is the relative angle made by the wind with
the wings
14
Relation between aoa lift
  • Angle of attack is directly proportional to the
    lift coefficient till a maximum limit which is
    generally about 17o
  • After which the plane stalls

15
Control Surfaces
16
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17
  • These are the surfaces which divert the direction
    of wind to provide change in direction of flight
  • There are basically three types of rotation of
    plane which provide the change in direction

18
Rotation of a plane
19
Turning the plane
  • The plane can be turned in right or left
    direction by using the ailerons to roll onto the
    side of movement and using the elevators to move
    up.
  • This can also be done by using the rudders

20
Channels
  • Generally a channel used to control a servo which
    decides a control surface and two servos are used
    for the ailerons leading to a 4-channel model
  • But amateurs can use a 3-channel which has only 1
    servo for the ailerons

21
Design Principles
22
Wing Loading
  • It is the ratio of the weight of the plane to the
    wing area
  • Gives a measure of the load given per unit area
    of the wing
  • Wing loading is an important factor which decides
    the balance between the forces

23
Aspect Ratio(AR)
  • Aspect Ratio is the ratio of square of
    wingspan to the area of the wing
  • AR l2 / A
  • Where l is the wingspan and A is the area of
    wing
  • Typical aspect ratios for gliders are 6-8

24
Powering the plane
25
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26
Motor specifications
  • After the thrust required is calculated the
    configuration of the motor is decided
  • The motor is selected by its KV rating which is
    basically the RPM per volt it can deliver
  • The KV rating is calculated by max current so
    while selecting a battery and ECS see to it that
    continuous current rating is greater than motor
    rating.

27
Typical motors
  • One of the usually motors used is the 2204 motor
    which provides about 350 gms of thrust
  • The thrust provided also depends upon the
    propellers used which is again specified by its
    pitch and diameter length.

28
Electronic control system(ECS)
  • Brushless DC motors do not have carbon brushes to
    have a constant direction of motion of the motor
  • So an ECS is used to provide switching action so
    that the polarity is changed and unidirectional
    rotatory motion is obtained.

29
Batteries
  • Usually Lithium Polymer batteries are used in
    aeromodels.
  • They come with voltage and current rating which
    must comply with our motor and ECS.

30
Another suggestion
  • A 1000mAh battery will provide power for approx.
    10 minutes in a 2204 motor.
  • But since the motor is going to be powered for
    only 30 secs a battery wit lesser power can be
    used which will reduce weight.

31
Electronic Components
32
Servo
  • They are motors with high torque and are used to
    control the control surfaces
  • They are decided by the required weight,torque,
    speed, dimensions

33
Receiver
  • It consists of receiver module and a antennae
    wire of about 2-3 feet long.
  • The receiver gets signal from the transmitter and
    then acts upon the servos
  • Nowadays there are ECSs which have separate power
    for the receiver so there is no need for separate
    power.

34
Transmitter
  • This consists of a hand console which sends
    signals according to the movement of a stick or
    switch
  • The frequency of the transmitter receiver is
    determined by a transducer crystal
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