mechanics Flashcards
Force of gravity between 2 masses
-(G*m1*m2/r²)
energy of gravity between 2 masses
-(G*m1*m2/r)
velocity with acceleration and displacement
v²=v0² + 2*a*Δd
distance with initial position, constant velocity and acceleration, and time
x = x0 + v0*t + 0.5*a*t²
velocity with acceleration and time
v = v0 + a*t
force of friction
F = F_normal*μ
centripetal acceleration
a_c = v²/r
Torque
τ = F*r*sin(ϴ) ϴ -> angle between position and force vectors
momentum
P = m*v
impulse
FΔt = ΔP
kinetic energy (motion)
KE = 1/2*m*v²
gravitational potential energy
U = m*g*h
work done on particle in motion with constant force
W = F*Δr*cos(ϴ)
Average power
P_avg = W/Δt
instantaneous power
P = F*v*cos(ϴ)
Force on a spring
F_k = -k*x
energy of a spring
U_k = 1/2*k*x²
period of a spring
T = 2*π*sqrt(m/k)
period of a pendulum
T = 2*π*sqrt(l/g)
general period form
T = 1/frequency
Linear momentum and angular momentum relationship
plinear=pangular/r
work-energy principle
Net work is equal to change in kinetic energy
Force and potential energy relationship
Fx = -dU/dx
elastic collision
total kinetic energy is conserved
inelastic collision
momentum is conserved, kinetic energy is not
final velocity for perfectly inelastic collision
vf = (m1v1i +m2v2i)/(m1 + m2)
final velocities for elastic collisions
v1f = [(m1 - m2)/(m1 + m2)]v1i + [2m2/(m1 + m2)]v2i
v2f = [2m1/(m1 + m2)]v1i + [(m2 - m1)/(m1 + m2)]v2i
center of mass for particles
xcm = (m1x1 + m2x2)/(m1 + m2)
center of mass for continuous solid
xcm = (1/Mtot) ∫x(m)dm
thrust from rocket
Fthrust = |ve*dM/dt|
- ve -> velocity of exhaust*
- dM/dt -> burn rate*
arc length
s = rθ
rotational kinematic equations
ωf = ωi + αt
θf = θi + ωit + 1/2αt2
ωf2 = ωi2 + 2α(θf - θi)
θf = θi + 1/2(ωi + ωf)t
Moment of Inertia
I = Σmiri2
rotational kinetic energy
KR = 1/2Iω2
I -> moment of inertia
parallel axis theorem
I = ICM + MD2
D -> distance from center of mass
torque
τ = Fd
torque and angular acceleration
τ = Iα
work-kinetic energy theorem for rotational motion
W = (1/2)Iωf2 - (1/2)Iωi2
angular momentum
L = mvrsinφ
φ -> angle between r and direction of linear momentum (direction of v)
angular momentum of rigid object
L = Iω
torque on rigid object
τ = Iα
Kepler’s first law
all planets move in elliptical orbits with sun at one focus
kepler’s second law
the radius vector drawn from sun to a planet sweeps out equal areas in equal time periods
kepler’s third law
T2 = (4π2/GMS)a3
- T -> period of rotation*
- a -> semimajor axis*
total energy for circular orbits
E = -(GMm)/(2r)
total energy for elliptical orbits
E = -(GMm)/(2a)
escape velocity
vesc = √[(2GME/RE)]