AP Physics 1 Full Review (Unit 5 - Unit 6)

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57 Terms

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Radian measure

s/r

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Angular position

Measured by angle θ

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Angular displacement

Change in θ (θfi)

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Rigid Body

Each point rotates with the same change in θ

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Angular Velocity Equation

ωavg (rad/s) = Δθ / Δt (rad/sec)

Average rate at which angular position changes

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Angular Acceleration Equation

αavg (rad/s²) = Δω / Δt (rad/s²)

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Connecting linear and angular displacement

Δs = rΔθ

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Connecting linear and angular velocity

v = rω

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Connecting tangential and angular acceleration

aT = rα

Tangential Acceleration = linear (speed kind of)

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Torque

When a force exerted on an object causes it to change rotational motion (turning effect)

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When does force exert torque?

For Force to exert torque, there needs to be a component of the force that is perpendicular to the radius of rotation

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The turning effect is dependent on __ distance?

radial

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Torque equation

τ = Iα

τ = rperpendicularF

τ = rFsinθ

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Free body diagram vs Force diagram

FBD: represents all forces acting on COM

Force Diagram: SHows forces acting on rigid object at the point of contact (shape instead of dot)

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Rotational Inertia

Resistance to change to rotation (I)

For rotational motion to change, torque must be exerted

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Rotational Inertia Equation

I = mr²

Itotal = Σ(mr²)i

Itotal = Ia + Ib

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Rotational Inertia depends on:

mass, size, and distribution of mass

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Coefficient of mass distribution

I = #mr²

# is given depending on mass distribution

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Rigid bodies usually rotate about ___

Center of Mass

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Parallel Axis Theorem

I’ = Icm = Md²

d = distance to the new axis point (ex. spinning a ruler from the farther hole rather than the middle)

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Translational Equilibrium

When FNET = 0

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Rotational Equilibrium

When τNET = 0

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Calculating net torque with multiple forces

Add them

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Directions in rotational kinematics

Usually (can choose):

Counterclockwise = +

Clockwise = -


Add CCW torques and subtract CW torques for rotational equilibrium

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Newton’s First Law regarding rotational motion

ω = constant if τNET = 0

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Newton’s 2nd Law regarding rotational motion

αsystem directly proportional to τNET

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Rotational inertia for disk (uniform mass)

Idisk = (1/2)mr²

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Acceleration of a massive pulley

αsystem = (m1-m2)g / (1/2)mpulley+m1+m2

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Acceleration of massless (ideal) pulley

αsystem = (m1 - m2)g / m1+m2

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Solving multi-object systems with a massive pulley requires ___

Newton’s 2nd Law for rotational motion

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Ideal Pulley

  • Has no mass (doesn’t affect system’s inertia)

  • Doesn’t disperse energy (No friction in axle)

  • Doesn’t change rope tension as it goes over the pulley

  • Assume tension is the same on both sides

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Angular Impulse Equation

J = τt

Torque x time

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Massive Pulley

  • Has rotational invertía

  • Some force goes into spinning, not just pulling objects

  • Tension is different on each side of the rope

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Reminder

Sum torques for rotating forces in system and set equal to Iα

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Translational Motion

Object moving in 1 or 2 dimensions (COM Moving)

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Rotational Kinetic Energy

Object moving but COM not moving

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Linear Kinematics —> Rotational Kinematics

x —> θ

v —> ω

a —> α

m —> I (Rotational inertia)

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Equation for rotational Kinetic Energy

Krot = ½ Iω²

Ktrans = ½ mv²

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Ktotal =

Ktotal = Ktrans + Krot (Scalar)

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“Rotational Analogs”

Rotational equivalents to linear

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Rotating objects have __ energy

Kinetic

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Work equation

W = τΔθ = ΔK

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Area under a τ v θ graph

Area = work done (like F v d)

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Work-Kinetic Energy Theorem

W = ΔKrot

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Angular Momentum equation

L = Iω (kgm²/s)

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Change in Angular Momentum equation

ΔL = ΣτΔt = IΔω

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Area under Angular Momentum v time graph (L v t)

Net Torque

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Rolling Rigid Bodies

Has both Ktrans and Krot

Ktotal = ½ mv² + ½ Iω²

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Rolling without slipping (x, v, and a of COM)

Δxcm = rΔθ

Vcm = rω

acm = rα

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Reminder

Rotating/rolling conserves energy (friction doesn’t dissipate energy in that case)

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Systems with more I have more __ in rotational

Ktotal

Ktrans < Krot

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Rolling with Slipping (Mechanical Energy)

Mechanical Energyfinal < Mechanical Energyinitial

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Velocity for orbiting satellite equation

v = Square root (GM/r)

M = mass of central body

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Kinetic energy of a satellite is __

constant

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Angular momentum in linear terms

L = rmvsinθ

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Elliptical Orbits

  • KE changes

  • GPE changes

  • Mechanical Energy constant

  • Angular momentum constant

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Escape velocity equation

Vesc = Square root (2GM/r)

Not on equation sheet, derived