3.2 Types of Motion and Fluid Mechanics
Linear Motion
movement of a bod in a straight or curved line, where all parts move the same distance in the same direction over the same time
a force is applied to the centre of mass of a body (direct force is applied)
Descriptors of linear motion
Descriptor | Definition | Calculation | Unit |
Distance | Measured | Metres | |
Displacement | The shortest straight line route from start to finish | Measured | Metres |
Speed | The rate of change in distance | Speed = distance/ time | Metres per second |
Velocity | T | Velocity = displacement/ time | Metres per second |
Acceleration/ deceleration | T | Acceleration = (final velocity- initial velocity)/ time | Metres per second per second |
Graphs of linear motion
Distance/Time
Speed/ Time
Velocity/ Time
Angular Motion
movement of a body or part of a body in a circular path about an axis of rotation
an eccentric force/ torque is applied to a body, outside of the centre of mass
Axes of rotation
Longitudinal - top to bottom
Transverse- side to side
Frontal- front to back
Descriptors of angular motion
Descriptor | Definition | Calculation | Unit |
Moment of Inertia | The resistance of a body to change its angular motion or rotation | MI = mass x distribution of mass from the axis of rotation² | Kilogram metres² |
Angular Velocity | The rate of change in angular displacement or rate of rotation | Angular velocity = angular displacement/ time | Radians per second |
Angular Momentum | The quantity of angular motion possessed by a body | Angular momentum = MI x angular velocity | Kilogram metres² per second |
Radians
the angle through which a body rotates
Radian = 57.3 degrees
6.28 rads in a circle
Factors affecting size of moment of inertia
Mass
greater mass = greater MI
the lower the mass, the easier it is to change the rate of rotation
sports with a high degree of rotation - e.g. high board diving - are often performed by athletes with a lower mass
Distribution of mass from the axis of rotation
the further away the mass is from the axis of rotation, the higher the MI
the more closely the mass is tucked in around the axis of rotation, the lower the MI
a back tuck is easier than a back layout
the body will face less resistance in the back tuck, so will rotate quicker
MI directly effects angular velocity:
high MI = high resistance to rotation = low angular velocity = rate of spin is slow
Conservation of angular momentum
angular momentum, once generated, does not change, unless an eccentric force is applied
remains constant, and is therefore called a conserved quantity
this is linked to the angular analogue of Newton’s first law
The Angular Analogue of Newton’s First Law states that a rotating body will continue to turn about an axis of rotation with constant angular momentum unless acted upon by an eccentric force
Practical Example
At take off, angular momentum is generated by the ice skater applying an eccentric force from the ice to the body. Rotation is about the longitudinal axis. Distribution of mass is away from the longitudinal axis, so MI is high, angular velocity is low and rate of spin is low. During flight, the mass is distributed closer to the axis of rotation, decreasing MI, increasing angular velocity, and increasing rate of spin. During landing, the mass is distributed further away from the axis of rotation, increasing MI, decreasing angular velocity, and decreasing rate of spin.
Graph of angular velocity
Applied to a diver
At take off, angular momentum is generated by an eccentric force from the springboard acting on the body.
Rotation occurs about the transverse axis.
Angular momentum is a conserved quantity and so will remain consistent throughout the movement.
The straight body position which the diver creates during take off distributes the mass away from the axis of rotation - MI is high, angular velocity and rate of spin are low, so the diver rotates slowly.
During flight, the diver will create a tucked body position, which distributes mass close to the axis of rotation - MI is decreased, angular velocity and rate of spin are increased, so the diver rotates quickly.
When the diver prepares to enter the water, they will create a straight body position, which distributes the mass away from the axis of rotation - MI is increased, angular velocity and rate of sin are decreased so the diver rotates slowly.
Projectile Motion
the movement of a body through the air following a curved flight path under the force of gravity
Factors affecting horizontal distance travelled
speed of release - the greater the force applied, the greater the change in momentum and therefore acceleration, so it will travel a grater distance
angle of release:
90 - accelerate vertically and come back down, travelling 0m
45 - optimal angle*
<45 - reaches peak height to quickly and rapidly returns to the ground
>45 - does not achieve sufficient height to maximise flight time
height of release
* 45 is only the optimal angle if the release and landing height are equal - e.g a golf ball
- if the landing height for the projectile is below release height (javelin and shot put), the optimal angle will be below 45
aerodynamic factors - Bernoulli and Magnus
Flight paths
Parabolic = uniform curve
if weight is the dominant force, with little air resistance
shot put, football, tennis ball
Non-parabolic = unsymmetrical curve
is air resistance is the dominant force, with little weight
shuttlecock, discus
Parallelogram of forces
considers the result of all forces acting on a projectile in flight
draw a free body diagram, add broken parallel lines, draw a diagonal line from CoM to opposite corner
if the resultant force is closer to weight it will be parabolic
if the resultant force is closer to air resistance it will be non-parabolic
Lift and Bernoulli
if an aerofoil is present, extra lift can be produced
the air parts as the aerofoil travels through the air, the air over the top flows faster than the air under the aerofoil so they meet at the same time
increased velocity = decreased pressure, so an area of low pressure forms above, and an area of high pressure forms below - creates a pressure gradient and additional lift force
optimal angle of attack = 17
Downwards lift force
apply Bernoulli’s principle with an inverted aerofoil
increases downwards force and helps hold an object, e.g a bike or F1 car, to the track
the spoiler forces air to travel underneath, which is further, and so needs a higher velocity, creating an area of low pressure below the spoiler, and an area of high pressure above the spoiler - creates a pressure gradient and additional downwards lift force
Spin and Magnus
topspin, backspin, hook, slice
the point at which the eccentric force is applied determined which way the object will spin
Topspin = applied above the centre of mass - rotates downwards - shortens flight path
Backspin = applied below the centre of mas - rotates upwards - lengthens the flight path
Hook = applied right of the centre of mass - rotates left - swerves to the left
Slice = applied left of the centre of mass - rotates right - swerves to the right
Topspin Example
top of the ball spins against the direction of airflow - creates low velocity and high pressure
bottom of the ball spins with the direction of airflow - high velocity and low pressure
creates a pressure gradient and a downwards magnus force from an area of high to low pressure
magnus force adds weight to the ball so the flight path shortens
Fluid Mechanics
There are four main factors which affect air resistance and drag.
Drag is the force that opposes the direction of motion of a body through water or air
Velocity - increased velocity = increased drag
Frontal cross-sectional area - greater cross-sectional area = greater drag
Streamlining and shape - more aerodynamic = lower drag
Surface characteristics - smoother surface = less drag