Caption: The calculation of center of mass illustrated.
Features:
The result is the center of mass---more explicitly the center-of-mass position vector.
Recall, a vector is a quantity with both a magnitude and a direction.
R_cm = ∑_i (m_i*R_i) / ∑_i (m_i) = ∑_i (m_i*R_i) / mwhere capital letters signify vectors, R_cm is the center of mass, i is an index for the bits, R_i is the position vector for bit i, m_i is the mass of bit i, and m is the system mass (i.e., the total mass).
F_net_ext = m*A_cm ,where F_net_ext is the net external force on the system, m is again the system mass, and A_cm is the center-of-mass acceleration.
So it's center-of-mass motion which is determined by F=ma---a point often neglected in high-school physics courses.
Center-of-mass (CM)
inertial frames
are discussed in Mechanics file:
frame_basics.html
and
Mechanics file:
frame_hierarchy_astro.html.
Proof:
Given a set of
point masses i
each with mass m_i
and m=∑_i m_i and
position vector R_i, the
center of mass R_cm is determined by
mR_cm = ∑_i m_i*R_i = ∑_j (∑_i m_i*R_i)_subset_j = ∑_j m_jR_cm_j ,
where there are a general set of subsets j of
point masses
and
m_j is the sum of the
mass of the subset j.
Clearly, R_cm_j is the center of mass
of the subset j.
Since the subsets are general,
the proof is complete:
QED.