Center of mass#Center of gravity

The concept of center of gravity or weight was studied extensively by the ancient Greek mathematician, physicist, and engineer Archimedes of Syracuse. He worked with simplified assumptions about gravity that amount to a uniform field, thus arriving at the mathematical properties of what we now call the center of mass. Archimedes showed that the torque exerted on a lever by weights resting at various points along the lever is the same as what it would be if all of the weights were moved to a single point—their center of mass. In his work On Floating Bodies, Archimedes demonstrated that the orientation of a floating object is the one that makes its center of mass as low as possible. He developed mathematical techniques for finding the centers of mass of objects of uniform density of various well-defined shapes.{{sfn|Shore|2008|pp=9–11}}

Other ancient mathematicians who contributed to the theory of the center of mass include Hero of Alexandria and Pappus of Alexandria. In the Renaissance and Early Modern periods, work by Guido Ubaldi, Francesco Maurolico,{{sfn|Baron|2004|pp=91–94}} Federico Commandino,{{sfn|Baron|2004|pp=94–96}} Evangelista Torricelli, Simon Stevin,{{sfn|Baron|2004|pp=96–101}} Luca Valerio,{{sfn|Baron|2004|pp=101–106}} Jean-Charles de la Faille, Paul Guldin,{{sfn|Mancosu|1999|pp=56–61}} John Wallis, Christiaan Huygens,{{Cite journal | last=Erlichson|first=H.|date=1996|title=Christiaan Huygens' discovery of the center of oscillation formula| url=https://aapt.scitation.org/doi/10.1119/1.18156|journal=American Journal of Physics|volume=64|issue=5| pages=571–574 |doi=10.1119/1.18156|bibcode=1996AmJPh..64..571E|issn=0002-9505}} Louis Carré, Pierre Varignon, and Alexis Clairaut expanded the concept further.{{sfn|Walton|1855|p=2}}

Newton's second law is reformulated with respect to the center of mass in Euler's first law.{{sfn|Beatty|2006|p=29}}

{{More citations needed section|date=September 2024}}

The center of mass is the unique point at the center of a distribution of mass in space that has the property that the weighted position vectors relative to this point sum to zero. In analogy to statistics, the center of mass is the mean location of a distribution of mass in space.

In the case of a system of particles {{math|1=P_i, i = 1, ..., n }}, each with mass {{mvar|m_i}} that are located in space with coordinates {{math|1=r_i, i = 1, ..., n }}, the coordinates R of the center of mass satisfy

$$\backslash sum\_\{i=1\}^n\; m\_i(\backslash mathbf\{r\}\_i\; -\; \backslash mathbf\{R\})\; =\; \backslash mathbf\{0\}.$$

Solving this equation for R yields the formula

$$\backslash mathbf\{R\}=\{\backslash sum\_\{i=1\}^n\; m\_i\; \backslash mathbf\{r\}\_i\backslash over\backslash sum\_\{i=1\}^n\; m\_i\; \}.$$

If the mass distribution is continuous with the density ρ(r) within a solid Q, then the integral of the weighted position coordinates of the points in this volume relative to the center of mass R over the volume V is zero, that is

$$\backslash iiint\_\{Q\}\; \backslash rho(\backslash mathbf\{r\})\; \backslash left(\backslash mathbf\{r\}\; -\; \backslash mathbf\{R\}\backslash right)\; dV\; =\; \backslash mathbf\{0\}.$$

Solve this equation for the coordinates R to obtain

$$\backslash mathbf\; R\; =\; \backslash frac\; 1\; M\; \backslash iiint\_\{Q\}\backslash rho(\backslash mathbf\{r\})\; \backslash mathbf\{r\}\; \backslash ,\; dV,$$

where M is the total mass in the volume.

If a continuous mass distribution has uniform density, which means that ρ is constant, then the center of mass is the same as the centroid of the volume.{{sfn|Levi|2009|p=85}}

{{Further|Barycentric coordinate system}}

The coordinates R of the center of mass of a two-particle system, P₁ and P₂, with masses m₁ and m₂ is given by

$$\backslash mathbf\{R\}\; =\; \{\{m\_1\; \backslash mathbf\{r\}\_1\; +\; m\_2\backslash mathbf\{r\}\_2\}\; \backslash over\; m\_1\; +\; m\_2\}.$$

Let the percentage of the total mass divided between these two particles vary from 100% P₁ and 0% P₂ through 50% P₁ and 50% P₂ to 0% P₁ and 100% P₂, then the center of mass R moves along the line from P₁ to P₂. The percentages of mass at each point can be viewed as projective coordinates of the point R on this line, and are termed barycentric coordinates. Another way of interpreting the process here is the mechanical balancing of moments about an arbitrary point. The numerator gives the total moment that is then balanced by an equivalent total force at the center of mass. This can be generalized to three points and four points to define projective coordinates in the plane, and in space, respectively.

For particles in a system with periodic boundary conditions two particles can be neighbours even though they are on opposite sides of the system. This occurs often in molecular dynamics simulations, for example, in which clusters form at random locations and sometimes neighbouring atoms cross the periodic boundary. When a cluster straddles the periodic boundary, a naive calculation of the center of mass will be incorrect. A generalized method for calculating the center of mass for periodic systems is to treat each coordinate, x and y and/or z, as if it were on a circle instead of a line.{{sfn|Bai|Breen|2008}} The calculation takes every particle's x coordinate and maps it to an angle,

$$\backslash theta\_i\; =\; \backslash frac\{x\_i\}\{x\_\backslash max\}\; 2\; \backslash pi$$

where x_max is the system size in the x direction and $x\_i\; \backslash in\; [0,\; x\_\backslash max)$. From this angle, two new points $(\backslash xi\_i,\; \backslash zeta\_i)$ can be generated, which can be weighted by the mass of the particle $x\_i$ for the center of mass or given a value of 1 for the geometric center:

$$\backslash begin\{align\}$$

\xi_i &= \cos(\theta_i) \\

\zeta_i &= \sin(\theta_i)

\end{align}

In the $(\backslash xi,\; \backslash zeta)$ plane, these coordinates lie on a circle of radius 1. From the collection of $\backslash xi\_i$ and $\backslash zeta\_i$ values from all the particles, the averages $\backslash overline\{\backslash xi\}$ and $\backslash overline\{\backslash zeta\}$ are calculated.

$$\backslash begin\{align\}$$

\overline{\xi} &= \frac 1 M \sum_{i=1}^n m_i \xi_i, \\

\overline{\zeta} &= \frac 1 M \sum_{i=1}^n m_i \zeta_i,

\end{align}

where {{mvar|M}} is the sum of the masses of all of the particles.

These values are mapped back into a new angle, $\backslash overline\{\backslash theta\}$, from which the x coordinate of the center of mass can be obtained:

$$\backslash begin\{align\}$$

\overline{\theta} &= \operatorname{atan2}\left(-\overline{\zeta}, -\overline{\xi}\right) + \pi \\

x_\text{com} &= x_\max \frac{\overline{\theta}}{2 \pi}

\end{align}

The process can be repeated for all dimensions of the system to determine the complete center of mass. The utility of the algorithm is that it allows the mathematics to determine where the "best" center of mass is, instead of guessing or using cluster analysis to "unfold" a cluster straddling the periodic boundaries. If both average values are zero, $\backslash left(\backslash overline\{\backslash xi\},\; \backslash overline\{\backslash zeta\}\backslash right)\; =\; (0,\; 0)$, then $\backslash overline\{\backslash theta\}$ is undefined. This is a correct result, because it only occurs when all particles are exactly evenly spaced. In that condition, their x coordinates are mathematically identical in a periodic system.

{{Refimprove section|date=September 2024}}

{{Redirect|Center of gravity}}

{{Main|Centers of gravity in non-uniform fields}}

File:CoG stable.svg

A body's center of gravity is the point around which the resultant torque due to gravity forces vanishes.Resnick, R. and Halliday, D. (1962) Physics, 9-1 “Center of Mass”, Wiley Where a gravity field can be considered to be uniform, the mass-center and the center-of-gravity will be the same. However, for satellites in orbit around a planet, in the absence of other torques being applied to a satellite, the slight variation (gradient) in gravitational field between closer-to and further-from the planet (stronger and weaker gravity respectively) can lead to a torque that will tend to align the satellite such that its long axis is vertical. In such a case, it is important to make the distinction between the center-of-gravity and the mass-center.Resnick, R. and Halliday, D. (1962) Physics, 14-3 “Center of Gravity”, Wiley Any horizontal offset between the two will result in an applied torque.

The mass-center is a fixed property for a given rigid body (e.g. with no slosh or articulation), whereas the center-of-gravity may, in addition, depend upon its orientation in a non-uniform gravitational field. In the latter case, the center-of-gravity will always be located somewhat closer to the main attractive body as compared to the mass-center, and thus will change its position in the body of interest as its orientation is changed.

In the study of the dynamics of aircraft, vehicles and vessels, forces and moments need to be resolved relative to the mass center. That is true independent of whether gravity itself is a consideration. Referring to the mass-center as the center-of-gravity is something of a colloquialism, but it is in common usage and when gravity gradient effects are negligible, center-of-gravity and mass-center are the same and are used interchangeably.

In physics the benefits of using the center of mass to model a mass distribution can be seen by considering the resultant of the gravity forces on a continuous body. Consider a body Q of volume V with density ρ(r) at each point r in the volume. In a parallel gravity field the force f at each point r is given by,

$$\backslash mathbf\{f\}(\backslash mathbf\{r\})\; =\; -dm\backslash ,\; g\backslash mathbf\{\backslash hat\{k\}\}\; =\; -\backslash rho(\backslash mathbf\{r\})\; \backslash ,\; dV\backslash ,g\backslash mathbf\{\backslash hat\{k\}\},$$

where dm is the mass at the point r, g is the acceleration of gravity, and $\backslash mathbf\{\backslash hat\{k\}\}$ is a unit vector defining the vertical direction.

Choose a reference point R in the volume and compute the resultant force and torque at this point,

$$\backslash mathbf\{F\}\; =\; \backslash iiint\_\{Q\}\; \backslash mathbf\{f\}(\backslash mathbf\{r\})\; \backslash ,\; dV\; =\; \backslash iiint\_\{Q\}\backslash rho(\backslash mathbf\{r\})\; \backslash ,\; dV\; \backslash left(\; -g\; \backslash mathbf\{\backslash hat\{k\}\}\backslash right)\; =\; -Mg\backslash mathbf\{\backslash hat\{k\}\},$$

and

$$\backslash mathbf\{T\}\; =\; \backslash iiint\_\{Q\}\; (\backslash mathbf\{r\}\; -\; \backslash mathbf\{R\})\; \backslash times\; \backslash mathbf\{f\}(\backslash mathbf\{r\})\; \backslash ,\; dV\; =\; \backslash iiint\_\{Q\}\; (\backslash mathbf\{r\}\; -\; \backslash mathbf\{R\})\; \backslash times\; \backslash left(-g\backslash rho(\backslash mathbf\{r\})\; \backslash ,\; dV\; \backslash ,\; \backslash mathbf\{\backslash hat\{k\}\}\backslash right)\; =\; \backslash left(\backslash iiint\_\{Q\}\; \backslash rho(\backslash mathbf\{r\})\; \backslash left(\backslash mathbf\{r\}\; -\; \backslash mathbf\{R\}\backslash right)\; dV\; \backslash right)\; \backslash times\; \backslash left(-g\backslash mathbf\{\backslash hat\{k\}\}\backslash right)\; .$$

If the reference point R is chosen so that it is the center of mass, then

$$\backslash iiint\_\{Q\}\; \backslash rho(\backslash mathbf\{r\})\; \backslash left(\backslash mathbf\{r\}\; -\; \backslash mathbf\{R\}\backslash right)\; dV\; =\; 0,$$

which means the resultant torque {{nowrap|1=T = 0}}. Because the resultant torque is zero the body will move as though it is a particle with its mass concentrated at the center of mass.

By selecting the center of gravity as the reference point for a rigid body, the gravity forces will not cause the body to rotate, which means the weight of the body can be considered to be concentrated at the center of mass.

The linear and angular momentum of a collection of particles can be simplified by measuring the position and velocity of the particles relative to the center of mass. Let the system of particles P_i, i = 1, ..., n of masses m_i be located at the coordinates r_i with velocities v_i. Select a reference point R and compute the relative position and velocity vectors,

$$\backslash mathbf\{r\}\_i\; =\; (\backslash mathbf\{r\}\_i\; -\; \backslash mathbf\{R\})\; +\; \backslash mathbf\{R\},\; \backslash quad\; \backslash mathbf\{v\}\_i\; =\; \backslash frac\{d\}\{dt\}(\backslash mathbf\{r\}\_i\; -\; \backslash mathbf\{R\})\; +\; \backslash mathbf\{v\}.$$

The total linear momentum and angular momentum of the system are

$$\backslash mathbf\{p\}\; =\; \backslash frac\{d\}\{dt\}\backslash left(\backslash sum\_\{i=1\}^n\; m\_i\; (\backslash mathbf\{r\}\_i\; -\; \backslash mathbf\{R\})\backslash right)\; +\; \backslash left(\backslash sum\_\{i=1\}^n\; m\_i\backslash right)\; \backslash mathbf\{v\},$$

and

$$\backslash mathbf\{L\}\; =\; \backslash sum\_\{i=1\}^n\; m\_i\; (\backslash mathbf\{r\}\_i\; -\; \backslash mathbf\{R\})\; \backslash times\; \backslash frac\{d\}\{dt\}(\backslash mathbf\{r\}\_i\; -\; \backslash mathbf\{R\})\; +\; \backslash left(\backslash sum\_\{i=1\}^n\; m\_i\; \backslash right)\; \backslash left[\backslash mathbf\{R\}\; \backslash times\; \backslash frac\{d\}\{dt\}(\backslash mathbf\{r\}\_i\; -\; \backslash mathbf\{R\})\; +\; (\backslash mathbf\{r\}\_i\; -\; \backslash mathbf\{R\})\; \backslash times\; \backslash mathbf\{v\}\; \backslash right]\; +\; \backslash left(\backslash sum\_\{i=1\}^n\; m\_i\; \backslash right)\backslash mathbf\{R\}\; \backslash times\; \backslash mathbf\{v\}$$

If R is chosen as the center of mass these equations simplify to

$$\backslash mathbf\{p\}\; =\; m\backslash mathbf\{v\},\backslash quad\; \backslash mathbf\{L\}\; =\; \backslash sum\_\{i=1\}^n\; m\_i\; (\backslash mathbf\{r\}\_i\; -\; \backslash mathbf\{R\})\; \backslash times\; \backslash frac\{d\}\{dt\}(\backslash mathbf\{r\}\_i\; -\; \backslash mathbf\{R\})\; +\; \backslash sum\_\{i=1\}^n\; m\_i\; \backslash mathbf\{R\}\; \backslash times\; \backslash mathbf\{v\}$$

where m is the total mass of all the particles, p is the linear momentum, and L is the angular momentum.

The law of conservation of momentum predicts that for any system not subjected to external forces the momentum of the system will remain constant, which means the center of mass will move with constant velocity. This applies for all systems with classical internal forces, including magnetic fields, electric fields, chemical reactions, and so on. More formally, this is true for any internal forces that cancel in accordance with Newton's third law.{{sfn|Kleppner|Kolenkow|1973|p=117}}

{{see also|Centroid#Determination}}

File:Center gravity 2.svg

The experimental determination of a body's center of mass makes use of gravity forces on the body and is based on the fact that the center of mass is the same as the center of gravity in the parallel gravity field near the earth's surface.

The center of mass of a body with an axis of symmetry and constant density must lie on this axis. Thus, the center of mass of a circular cylinder of constant density has its center of mass on the axis of the cylinder. In the same way, the center of mass of a spherically symmetric body of constant density is at the center of the sphere. In general, for any symmetry of a body, its center of mass will be a fixed point of that symmetry.[https://feynmanlectures.caltech.edu/I_19.html#Ch19-S1-p3 The Feynman Lectures on Physics Vol. I Ch. 19: Center of Mass; Moment of Inertia]

An experimental method for locating the center of mass is to suspend the object from two locations and to drop plumb lines from the suspension points. The intersection of the two lines is the center of mass.{{sfn|Kleppner|Kolenkow|1973|pp=119–120}}

The shape of an object might already be mathematically determined, but it may be too complex to use a known formula. In this case, one can subdivide the complex shape into simpler, more elementary shapes, whose centers of mass are easy to find. If the total mass and center of mass can be determined for each area, then the center of mass of the whole is the weighted average of the centers.{{sfn|Feynman|Leighton|Sands|1963|pp=19.1–19.2}} This method can even work for objects with holes, which can be accounted for as negative masses.{{sfn|Hamill|2009|pp=20–21}}

A direct development of the planimeter known as an integraph, or integerometer, can be used to establish the position of the centroid or center of mass of an irregular two-dimensional shape. This method can be applied to a shape with an irregular, smooth or complex boundary where other methods are too difficult. It was regularly used by ship builders to compare with the required displacement and center of buoyancy of a ship, and ensure it would not capsize.{{cite web|title=The theory and design of British shipbuilding |page=3 |url=http://www.ebooksread.com/authors-eng/amos-lowrey-ayre/the-theory-and-design-of-british-shipbuilding-hci/page-3-the-theory-and-design-of-british-shipbuilding-hci.shtml|work=Amos Lowrey Ayre|access-date=20 August 2012}}{{sfn|Sangwin|2006|p=7}}

An experimental method to locate the three-dimensional coordinates of the center of mass begins by supporting the object at three points and measuring the forces, F₁, F₂, and F₃ that resist the weight of the object, $\backslash mathbf\{W\}\; =\; -W\backslash mathbf\{\backslash hat\{k\}\}$ ($\backslash mathbf\{\backslash hat\{k\}\}$ is the unit vector in the vertical direction). Let r₁, r₂, and r₃ be the position coordinates of the support points, then the coordinates R of the center of mass satisfy the condition that the resultant torque is zero,

$$\backslash mathbf\{T\}\; =\; (\backslash mathbf\{r\}\_1\; -\; \backslash mathbf\{R\})\; \backslash times\; \backslash mathbf\{F\}\_1\; +\; (\backslash mathbf\{r\}\_2\; -\; \backslash mathbf\{R\})\; \backslash times\; \backslash mathbf\{F\}\_2\; +\; (\backslash mathbf\{r\}\_3\; -\; \backslash mathbf\{R\})\; \backslash times\; \backslash mathbf\{F\}\_3\; =\; 0,$$

or

$$\backslash mathbf\{R\}\; \backslash times\; \backslash left(-W\backslash mathbf\{\backslash hat\{k\}\}\backslash right)\; =\; \backslash mathbf\{r\}\_1\; \backslash times\; \backslash mathbf\{F\}\_1\; +\; \backslash mathbf\{r\}\_2\; \backslash times\; \backslash mathbf\{F\}\_2\; +\; \backslash mathbf\{r\}\_3\; \backslash times\; \backslash mathbf\{F\}\_3.$$

This equation yields the coordinates of the center of mass R* in the horizontal plane as,

$$\backslash mathbf\{R\}^*\; =\; -\backslash frac\{1\}\{W\}\; \backslash mathbf\{\backslash hat\{k\}\}\; \backslash times\; (\backslash mathbf\{r\}\_1\; \backslash times\; \backslash mathbf\{F\}\_1\; +\; \backslash mathbf\{r\}\_2\; \backslash times\backslash mathbf\{F\}\_2\; +\; \backslash mathbf\{r\}\_3\; \backslash times\; \backslash mathbf\{F\}\_3).$$

The center of mass lies on the vertical line L, given by

$$\backslash mathbf\{L\}(t)\; =\; \backslash mathbf\{R\}^*\; +\; t\backslash mathbf\{\backslash hat\{k\}\}.$$

The three-dimensional coordinates of the center of mass are determined by performing this experiment twice with the object positioned so that these forces are measured for two different horizontal planes through the object. The center of mass will be the intersection of the two lines L₁ and L₂ obtained from the two experiments.

{{Unreferenced section|date=September 2024}}

Engineers try to design a sports car so that its center of mass is lowered to make the car handle better, which is to say, maintain traction while executing relatively sharp turns.

The characteristic low profile of the U.S. military Humvee was designed in part to allow it to tilt farther than taller vehicles without rolling over, by ensuring its low center of mass stays over the space bounded by the four wheels even at angles far from the horizontal.

{{Main|Center of gravity of an aircraft}}

The center of mass is an important point on an aircraft, which significantly affects the stability of the aircraft. To ensure the aircraft is stable enough to be safe to fly, the center of mass must fall within specified limits. If the center of mass is ahead of the forward limit, the aircraft will be less maneuverable, possibly to the point of being unable to rotate for takeoff or flare for landing.{{sfn|Federal Aviation Administration|2007|p=1.4}} If the center of mass is behind the aft limit, the aircraft will be more maneuverable, but also less stable, and possibly unstable enough so as to be impossible to fly. The moment arm of the elevator will also be reduced, which makes it more difficult to recover from a stalled condition.{{sfn|Federal Aviation Administration|2007|p=1.3}}

For helicopters in hover, the center of mass is always directly below the rotorhead. In forward flight, the center of mass will move forward to balance the negative pitch torque produced by applying cyclic control to propel the helicopter forward; consequently a cruising helicopter flies "nose-down" in level flight.{{cite web | url=http://www.ultraligero.net/Cursos/helicoptero/Introduccion_a_la_aerodinamica_del%20_helicoptero.pdf | title=Helicopter Aerodynamics | access-date=23 November 2013 | pages=82 | url-status=dead | archive-url=https://web.archive.org/web/20120324063720/http://www.ultraligero.net/Cursos/helicoptero/Introduccion_a_la_aerodinamica_del%20_helicoptero.pdf | archive-date=24 March 2012 }}

{{Main|Barycenter}}File:orbit3.gif (red cross)]]

The center of mass plays an important role in astronomy and astrophysics, where it is commonly referred to as the barycenter. The barycenter is the point between two objects where they balance each other; it is the center of mass where two or more celestial bodies orbit each other. When a moon orbits a planet, or a planet orbits a star, both bodies are actually orbiting a point that lies away from the center of the primary (larger) body.{{sfn|Murray|Dermott|1999|pp=45–47}} For example, the Moon does not orbit the exact center of the Earth, but a point on a line between the center of the Earth and the Moon, approximately 1,710 km (1,062 miles) below the surface of the Earth, where their respective masses balance. This is the point about which the Earth and Moon orbit as they travel around the Sun. If the masses are more similar, e.g., Pluto and Charon, the barycenter will fall outside both bodies.

Knowing the location of the center of gravity when rigging is crucial, possibly resulting in severe injury or death if assumed incorrectly. A center of gravity that is at or above the lift point will most likely result in a tip-over incident. In general, the further the center of gravity below the pick point, the safer the lift. There are other things to consider, such as shifting loads, strength of the load and mass, distance between pick points, and number of pick points. Specifically, when selecting lift points, it is very important to place the center of gravity at the center and well below the lift points.{{Cite web |url=https://www.fema.gov/pdf/emergency/usr/module4.pdf |title=Structural Collapse Technician: Module 4 - Lifting and Rigging |access-date=27 November 2019 |website=FEMA.gov }}

{{Main|Kinesiology}}{{anchor|Kinesiology}}

The center of mass of the adult human body vertically is 10 cm above the trochanter (the femur joins the hip),{{Cite journal |last=Palmer |first=Carroll E. |date=1944 |title=Studies of the Center of Gravity in the Human Body |url=https://www.jstor.org/stable/1125537 |journal=Child Development |volume=15 |issue=2/3 |pages=99–180 |doi=10.2307/1125537|jstor=1125537 }} with it in horizontally being located 1.4 cm forward of the knee, and 1.0 behind the trochanter.{{Cite journal |last1=Woodhull |first1=A. M. |last2=Maltrud |first2=K. |last3=Mello |first3=B. L. |date=1985 |title=Alignment of the human body in standing |url=http://link.springer.com/10.1007/BF00426309 |journal=European Journal of Applied Physiology and Occupational Physiology |language=en |volume=54 |issue=1 |pages=109–115 |doi=10.1007/BF00426309 |pmid=4018044 |issn=0301-5548}} In kinesiology and biomechanics, the center of mass is an important parameter that assists people in understanding their human locomotion. Typically, a human's center of mass is detected with one of two methods: the reaction board method is a static analysis that involves the person lying down on that instrument, and use of their static equilibrium equation to find their center of mass; the segmentation method relies on a mathematical solution based on the physical principle that the summation of the torques of individual body sections, relative to a specified axis, must equal the torque of the whole system that constitutes the body, measured relative to the same axis.{{sfn|Vint|2003|pp=1–11}}

The Center-of-gravity method is a method for convex optimization, which uses the center-of-gravity of the feasible region.

{{Portal|Physics}}

{{div col|colwidth=20em}}

• Barycenter
• Buoyancy
• Center of percussion
• Center of pressure (fluid mechanics)
• Center of pressure (terrestrial locomotion)
• Centroid
• Circumcenter of mass
• Expected value
• Mass point geometry
• Metacentric height
• Roll center
• Weight distribution

{{div col end}}

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{{Wiktionary|barycenter}}

• [https://web.archive.org/web/20050212113330/http://www.kettering.edu/~drussell/Demos/COM/com-a.html Motion of the Center of Mass] shows that the motion of the center of mass of an object in free fall is the same as the motion of a point object.
• [http://orbitsimulator.com/gravity/articles/ssbarycenter.html The Solar System's barycenter], simulations showing the effect each planet contributes to the Solar System's barycenter.

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Category:Classical mechanics

Category:Mass

Mass

Category:Moment (physics)