Nomenclature |
Nomenclature |
a = acceleration (m/s2) F = force (N = kg m/s2) |
a = acceleration (m/s2) F = force (N = kg m/s2) |
p = momentum (kg m/s) s = position (m) |
p = momentum (kg m/s) s = position (m) |
v = velocity (m/s) v0 = velocity at time t=0 |
v = velocity (m/s) v0 = velocity at time t=0 |
x(t) = position at time t x0 = position at time t=0 |
s(t) = position at time t s0 = position at time t=0 runit = unit vector pointing from the origin in polar coordinates θunit = unit vector pointing in the direction of increasing values of theta in polor coordinates |
Defining Equations Velocity |
Note: All quantities in bold represent vectors. |
v = δs/δt = ds/dt Acceleration |
Defining Equations |
a = δv/δt = dv/dt = d2s/dt2 |
Center of Mass |
Centripetal Acceleration |
n sCM = (∑misi)/mtotal i=0 where n is the number of mass particles. |
ac = v2 / R Momentum |
or: |
p = mv |
sCM = (∫sρ(s)dV)/mtotal |
Angular Momentum |
where ρ(s) is the scalar mass density as a function of the position vector. |
L = mvr |
Velocity |
Vector form L = pxR |
vaverage = Δs/Δt v = ds/dt |
R is the radius vector Force |
Acceleration |
F = dp/dt = d(mv)/dt |
aaverage = Δv/Δt a = dv/dt = d2s/dt2 |
F = ma (Constant Mass) Impulse |
*Centripetal Acceleration |
I = FΔt |
|ac| = ω2R = v2 / R (R = radius of the circle, ω = v/R [angular velocity]) |
Energy |
Momentum |
Kinetic Energy |
p = mv |
KE = 1/2 mv2 |
Force |
Potential Energy |
∑F = dp/dt = d(mv)/dt |
PE = mgh (near the earth's surface) |
∑F = ma (Constant Mass)ImpulseJ = Δp = ∫Fdt J = FΔt if F is constant Moment of IntertiaFor a single axis of rotation: Angular Momentum|L| = mvr iff v is perpendicular to r Vector form: L = r×p = Iω (Note: I can be treated like a vector if it is diagonalized first, but it is actually a 3×3 matrix) r is the radius vector Torque∑τ = dL/dt ∑τ = r×F if |r| and the sine of the angle between r and p remains constant. ∑τ = Iα This one is very limited, more added later. α = dω/dt Precession ===Energy === ΔKE = ∫Fnet·ds KE = ∫v·dp = 1/2 mv2 if m is constant PEdue to gravity = mgh (near the earth's surface) |
Useful derived equations |
Central Force Motion ===Useful derived equations == <ul> |
Position of an accelerating body |
s(t) = 1/2at2 + v0t + s0 if a is constant. |
x(t) = 1/2at2 + v0t + x0 |
|
Equation for velocity v2=v02 + 2aΔx |
v2=v02 + 2a·Δs |
where Δx is the change is position. |
</ul> |
Someone please add the equations for gravitational, electric, and magnetic forces |
/Talk |
a = acceleration (m/s2)
F = force (N = kg m/s2)
KE = kinetic energy (J = kg m2/s2)
m = mass (kg)
p = momentum (kg m/s)
s = position (m)
t = time (s)
v = velocity (m/s)
v0 = velocity at time t=0
W = work (J = kg m2/s2)
s(t) = position at time t
s0 = position at time t=0
runit = unit vector pointing from the origin in polar coordinates
θunit = unit vector pointing in the direction of increasing values of theta in polor coordinates
Note: All quantities in bold represent vectors.
nsCM = (∑misi)/mtotal
i=0where n is the number of mass particles.
or:
sCM = (∫sρ(s)dV)/mtotal
where ρ(s) is the scalar mass density as a function of the position vector.
vaverage = Δs/Δt
v = ds/dt
aaverage = Δv/Δt
a = dv/dt = d2s/dt2
|ac| = ω2R = v2 / R (R = radius of the circle, ω = v/R [angular velocity])
p = mv
∑F = dp/dt = d(mv)/dt
∑F = ma (Constant Mass)
J = Δp = ∫Fdt
J = FΔt if F is constant
For a single axis of rotation:
|L| = mvr iff v is perpendicular to r
Vector form:
L = r×p = Iω
(Note: I can be treated like a vector if it is diagonalized first, but it is actually a 3×3 matrix)
r is the radius vector
∑τ = dL/dt
∑τ = r×F if |r| and the sine of the angle between r and p remains constant.
∑τ = Iα This one is very limited, more added later. α = dω/dt
ΔKE = ∫Fnet·ds
KE = ∫v·dp = 1/2 mv2 if m is constant
PEdue to gravity = mgh (near the earth's surface)
g is the acceleration due to gravity, one the physical constants.
s(t) = 1/2at2 + v0t + s0 if a is constant.
v2=v02 + 2a·Δs