Mod 5 Advanced Mechanics Flashcards
What is non-unifrom circular motion
Circular motion where the speed of the object changes as it moves around a fixed path
What cause non-uniform circular motion
The net force is chaging in magnitude and in direction and hence does not provide required centripetal force (radial force)
What two components form net force in non-uniform circular motion
- Centripetal force
- Tangential force
Is net force constant in unifrom circular motion
Yes, since net force is centripetal force towards centre of circle
When a rocket is launched into a LEO how does its energy change during the journey
The rockets total mechanical energy (E= U + K) increases since work is done on rocket through use of thrusters to burn fuel
What 2 equations are equated to find orbital velocity
- F = mv^2/r
- F = GMm/r^2
Why don’t AC induction motors need brushes or slip rings
Current in the squirrel cage rotor is induced through three phase AC power supply not directly supplied
How do you prove that projectile motion is parabolic
- Through showing that equations of motion are in the form:
- y = ax^2+bx+c
What is the general process for solving projectile motion questions
- What is the value of g (are we on Earth)
- Do we have u(y)
- No –> find u(y) first
- Yes –> Try to solve by analysing vertical motion and use equations of motion
- if No find time using s(x) = u(x)t
What are the forces acting on an object on a banked track
- Normal force to track
- weight force mg directly down
- Acceration towards centre
Why are objects able to travel around banked tracks without any sideway force on the wheels by the track
- The normal force is tilted as a result of the banking
- Therefore a component of the normal force towards the centre of rotation exists and acts as a centripetal force required to execute a circular motion hence sideway force is not required
How is energy required to transfer to a new orbit calculated
- W = E(orbit)f-E(orbit)i
How is total mechanical energy of a satellite in orbit calculated
- E = U + K
- E = -GMm/r + 1/2(mv^2)
- E = -GMm/r + 1/2 m(GM/r)
- E = - 1/2 (GMm/r)
What impact does a chnage in mass of a space probe have on its motion
- r^3/T^2 = constant
- independent of mass of orbiting probe
- Any change in mass will not affect ratio hence if altitude remains the same then orbital period remains the same
- Speed is given by v = 2(pi)r/T since r and T do not change orbital velocity remains constant
How is escape velocity calculated
- When E = U + K = 0
- Hence 1/2mv^2 - GMm/r = 0
- 1/2v^2 = GM/r
- Vesc = sqrt(2GM/r)