module 5: advanced mechanics Flashcards

1
Q

What is a projectile?

A

A projectile is an object that is moving freely under the influence of gravity.
* For an object to be a projectile, there must be no force other than the gravitational force acting on the object.
* The net force on the projectile is the gravitational force (its weight).

The trajectory of a projectile follows a parabolic path.

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2
Q

Horizontal component of projectile motion

A

Horizontal Motion is constant velocity motion, the velocity is the same as the horizontal component of the initial velocity.

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3
Q

Vertical component of projectile motion

A

Vertical motion is uniform accelerated motion, the projectile experiences a constant downward acceleration due to gravity.

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4
Q

Projectile situation 1:

Launched from an elevated position and follows a parabolic path to the ground

A
  • Initial velocity is only in the horizontal direction (Initial velocity = horizontal velocity).
  • Velocity direction does not have initial velocity (initial vertical velocity = 0 ms-1).
  • Launch angle 𝜃 = 0°
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5
Q

Projectile situation 2:

Launched at an angle, rising upward to a peak before falling back down

A
  • Total vertical displacement = 0
  • When y is at maximum height, v = 0 ms-1
  • Initial speed = final speed
  • Time to rise = time to fall
  • Initial angle = final angle
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6
Q

Projectile situation 3:

Launched at an angle from an elevated position

A
  • Total vertical displacement = difference in height between the two levels
  • When y is at maximum height, v = 0 ms-1
  • Time to rise ≠ time to fall
  • Initial speed ≠ final speed
  • Initial angle ≠ final angle
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6
Q

Circular motion

A

For an object to move in a circular path, it must continually change the direction its travelling, hence circular motion requires a net force to be applied on the object.

Uniform circular motion refers to objects that move in a circle at constant speed.

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7
Q

Centipetal force

A

Centripetal force is the force that causes an object to move in a circular path and is directed towards the centre of the circle.

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8
Q

Tangential Velocity

A

Tangential velocity is the velocity of an object experiencing uniform circular motion.
* Tangential velocity of an object undergoing circular motion is related to the radius of the circle and the time it takes the object to complete one revolution.

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9
Q

Tangential Velocity equation

A

v = 2πr/T

Where:
v is the tangential velocity (ms-1)
r is the radius (m)
T is the period of rotation i.e. the time to go around the circle once (s)

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10
Q

Centripetal Accleration equation

A

ac = v^2 / r

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11
Q

Centripetal Force

A

Any motion in a curved path represents accelerated motion and requires a force directed towards the centre of curvature of the path.
* This force is called centripetal force which means “centre seeking” force.

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12
Q

Centripetal Force equation

A

FCentripetal = mv^2 / r

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13
Q

Unbanked curve

A

On an unbanked curve, the static frictional force from the car tires provides the centripetal force.
* If the frictional force is less than the centripetal force required, then the car cannot maintain its circular path and the car will skid at a tangent to the circle.

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14
Q

Banked curve

A

When the curve is banked, the centripetal force can be partially or entirely supplied by the horizontal component of the normal force.
* A reason to have banked curves would be to decrease the reliance on the force of friction.
* For every banked curve, there is one ideal speed (regardless of mass).

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15
Q

Ideal speed

A

When centripetal force is entirely supplied by the horizontal component of the normal force, it is called ‘ideal speed’.
* Speed of car > ideal speed, car will slide up inclined plane.
* Speed of car < ideal speed, car will slide down inclined plane.

16
Q

Angular acceleration

A

In UCM, angular velocity (⍵) is constant.
* If ⍵ changes with time, angular speed is increasing or decreasing, therefore angular acceleration is present
* For an object to start rotating around an axis, it requires a force to give the object some angular acceleration.

17
Q

Torque

A

Torque is the rotational equivalent of linear force, it is a vector quantity.
* Occurs when a force, F, is applied at some displacement, r, from an axis of rotation
* The direction of the torque is perpendicular to the plane of rotation, and the direction is determined using the right hand
* Have to indicate whether the torque turns the object clockwise or anticlockwise

18
Q

Properties of ellipses

A
  1. An ellipse is defined by two focal points, together called foci.
    * The sum of the distances to the foci from any point on the ellipse is always constant.
  2. The amount of flattening of the ellipse is called the eccentricity.
    * If e = 0, it’s a circle.
    * If e = 1, it’s a parabola
    * All ellipses have eccentricity in the range: 0 ≤ e ≤ 1.
  3. The longest axis of the ellipse is that major axis while the short is called the minor axis.
    * Half the major axis is termed a semi-major axis.
19
Q

Kepler’s First Law - Law of ellipses/Law of orbits

A

First law: The planet orbits the sun in elliptical orbits, with the Sun as one of the focal points.

20
Q

Kepler’s Second Law - Law of equal areas

A

Second law: the line between a planet and the sun (the radius vector) sweeps out equal areas in equal periods of time.

21
Q

Kepler’s Third Law - Law of Periods

A

Third law: The square of a planet’s period, T, is directly proportional to the cube of the semi-major axis of its orbit.

22
Q

Orbit characteristics

A

Orbits must be:
* Centred on the centre of the mass of the central object
* Elliptical or circular
Orbit characteristics are:
* Altitude (circular or near circular)
* Nearest and furthest point (e.g. perigee and apogee, if elliptical)
* Inclination (relative to the equator)

23
Q

Satellite definition

A

A satellite is an object that orbits a central body.
* A manufactured satellite is called an artificial satellite.
* Planets, asteroids, comets etc. are called natural satellites.

24
Q

Low Earth Orbits (LEO)

A

LEOs are slowed slightly by drag from the upper atmosphere, consequently called degenerate orbits as LEO satellites will eventually spiral back into the atmosphere.

Usually burns up during re-entry.

25
Q

LEO characteristics

A

Altitude: 160 and 2000 km
Orbital period: 128 minutes or less
Mean velocity to remain in orbit: 7.8 km/s
Used to measure a wide range of parameters such as ocean currents, temperature, icecap coverage, weather prediction (polar orbits) and satellite imaging.

26
Q

Middle Earth Orbits

A

Altitude: 2000 - 35786 km
Used for navigation (GPS) and communication

27
Q

Geosynchronous Earth Orbit

A

A geosynchronous orbit (GSO) is a high Earth orbit that allows satellites to match Earth’s rotation.
* Located 35,786 km above the Earth’s equator, is a valuable spot for monitoring weather, communications and surveillance.
* Has an orbital of 24 hours.

28
Q

Geostationary Earth Orbit

A

A geostationary orbit is a type of GSO that is equatorial, meaning that they remains above one point on the equator as the Earth rotates.
* Has an orbital of 24 hours.

29
Q

Escape Velocity

A

Escape velocity is the minimum velocity with which an object can escape the gravitational pull of the planet