Classical Mechanics: Newton's Laws and Universal Gravitation

Newton’s Laws of Motion - Introduction and Framework

  • Historical and Academic Context:     * The lecture notes are dated Wednesday, 25th April 2006.     * Newton’s laws of motion are celebrated for their extraordinary success, both in the breadth and depth of their applications.     * These laws have survived essentially intact for more than three centuries.     * The same longevity applies to Newton’s universal law of gravitation, which specifies the force all masses exert upon each other.
  • Scope and Foundation:     * Taken together, Newton’s laws represent virtually the entire foundation of classical mechanics.     * They provide an accurate explanation for a vast range of phenomena, from the behavior of large molecules to the movement of entire galaxies.     * These are laws of physics founded upon experimental evidence. Their validity stands or falls according to the accuracy of their predictions.
  • Dynamics vs. Kinematics:     * Kinematics: Concerned purely with the geometry of motion.     * Dynamics: Seeks to answer questions regarding what motion occurs when specified forces act upon a body.     * Newton’s laws of motion provide the rules that make the connection between force and the resulting motion.

The First Law of Motion (The Law of Inertia)

  • Conceptual Definition:     * The essence of Newton’s First Law is the concept of inertia.     * The law states that a body remains in a state of rest or continues to move with a constant velocity unless acted upon by an external force.
  • Inertial Reference Frames:     * In Newtonian mechanics, the stage of mechanics consists of a framework known as a reference frame.     * A reference frame in which the First Law of Newton is true is called an Inertial Frame.     * A frame moving with a constant velocity relative to an inertial frame is also an inertial frame.     * Consequently, there are infinitely many inertial frames.     * In practice, exact inertial frames are not available. Historically, frames were often defined with respect to the "fixed stars."
  • Practical Examples and Exercises:     * Question: Which of the following are inertial frames?         1. A frame fixed to a motor vehicle moving with constant speed around a flat circular track.         2. A frame fixed to a car traveling along a straight road while accelerating with constant acceleration.         3. A frame fixed to a car moving with constant speed up a road with a constant gradient.     * Solution: Only the third scenario (constant speed up a constant gradient) constitutes an inertial frame, as there is no acceleration involved (moving with constant velocity).

The Second Law of Motion (The Law of Motion)

  • Central Postulate:     * In an inertial frame, if a particle of mass mm is acted on by a force F\mathbf{F}, then:         F=dpdt\mathbf{F} = \frac{d\mathbf{p}}{dt}
  • Linear Momentum:     * The term p=mv\mathbf{p} = m\mathbf{v} is defined as the linear momentum of the particle, measured relative to the given inertial frame.
  • Significance:     * This equation provides the means of determining the trajectory of a particle and is known as the "Law of Motion."

The Third Law of Motion

  • Postulate of Interaction:     * The theory of motion is completed by postulating the nature of interaction between any two particles.     * If F12\mathbf{F}_{12} is the force that particle one (P1P_1) exerts on particle two (P2P_2), and F21\mathbf{F}_{21} is the force that P2P_2 exerts on P1P_1, then:         F12=F21\mathbf{F}_{12} = -\mathbf{F}_{21}
  • Core Principle:     * The mutual actions between particles are always equal in magnitude and opposite in direction.

Multi-Particle Systems and Center of Mass

  • Extension of the Laws:     * The standard formulation is extended to a system of NN particles.     * Let mim_i denote the mass and ri\mathbf{r}_i denote the position vector of the i$th particle (where i = 1, 2, \dots, N).\n    * The momentum of the i$th particle relative to an inertial frame is pi=midridt\mathbf{p}_i = m_i \frac{d\mathbf{r}_i}{dt}.     * The equations of motion are given by:         Fi=dpidt\mathbf{F}_i = \frac{d\mathbf{p}_i}{dt}
  • Force Categorization:     * FiF_i is the total force on the particle, which is the vector sum of inter-particle forces and external forces.     * Inter-particle forces (Fji\mathbf{F}_{ji}): Forces exerted on particle ii by other particles jj within the system.     * External forces (Fi(e)\mathbf{F}_i^{(e)}): Forces associated with sources outside the system.     * Total force equation:         Fi=jiFji+Fi(e)\mathbf{F}_i = \sum_{j \neq i} \mathbf{F}_{ji} + \mathbf{F}_i^{(e)}
  • N-Particle Equations of Motion:     * If masses mim_i are constant:         mid2ridt2=jiFji+Fi(e)m_i \frac{d^2\mathbf{r}_i}{dt^2} = \sum_{j \neq i} \mathbf{F}_{ji} + \mathbf{F}_i^{(e)}     * This represents a set of NN-coupled differential equations.
  • Center of Mass Definition:     * The center of mass of a system of particles (with masses m1,m2,,mNm_1, m_2, \dots, m_N and position vectors r1,r2,,rN\mathbf{r}_1, \mathbf{r}_2, \dots, \mathbf{r}_N) is a single point in space with position vector R\mathbf{R}, defined as:         R=1Mi=1Nmiri\mathbf{R} = \frac{1}{M} \sum_{i=1}^N m_i \mathbf{r}_i     * Where M=i=1NmiM = \sum_{i=1}^N m_i is the total mass of the system.     * The center of mass is the weighted mean of the position vectors where the weights are the particle masses.     * Examples:         1. Pair of Particles (P1,P2P_1, P_2): The center of mass is R=m1r1+m2r2m1+m2\mathbf{R} = \frac{m_1 \mathbf{r}_1 + m_2 \mathbf{r}_2}{m_1 + m_2}. It lies on the line joining P1P_1 and P2P_2 and divides the line in the ratio m2:m1m_2:m_1.         2. Three Identical Particles (P1,P2,P3P_1, P_2, P_3): The center of mass is R=r1+r2+r33\mathbf{R} = \frac{\mathbf{r}_1 + \mathbf{r}_2 + \mathbf{r}_3}{3}. This corresponds to the centroid of the triangle formed by the three particles.

Newton’s Universal Law of Gravitation

  • Basic Observation:     * Any object with mass attracts any other object with mass with a force called gravitation.
  • Formal Definition:     * The gravitational force that two particles exert on each other has a magnitude determined by:         F=Gm1m2R2F = \frac{Gm_1 m_2}{R^2}     * Where m1m_1 and m2m_2 are the particle masses, and RR is the distance between them.
  • The Gravitational Constant (GG):     * GG is a universal constant of gravitation.     * It is not dimensionless; its numerical value depends on the units used for mass, length, and force.     * In SI units:         G=6.67×1011Nm2kg2G = 6.67 \times 10^{-11} \, N \cdot m^2 \cdot kg^{-2}
  • Interaction Properties:     * Per Newton's Third Law, interaction forces are equal in magnitude, opposite in direction, and parallel to the straight line joining the particles.

Gravitational Force by Mass Distributions

  • Principle of Multiple Interaction:     * The effective force exerted on a particle is the resultant (vector sum) of the individual forces of interaction exerted on that particle by all other mass elements.
  • Example: Particle Attracted by Two Masses (A and B):     * Consider a particle CC of mass mm attracted by two particles AA and BB, each of mass MM, separated by a distance 2a2a. Let CC be at a distance xx from the midpoint DD of line ABAB.     * The distance from AA or BB to CC is R=a2+x2R = \sqrt{a^2 + x^2}.     * The force magnitude from one particle is F=GmMR2F' = \frac{GmM}{R^2}.     * By symmetry, the resultant force points toward DD along the x-x direction.     * The total magnitude is F=2Fcos(α)F = 2F' \cos(\alpha), where cos(α)=xR\cos(\alpha) = \frac{x}{R}.     * Resultant force:         F=2GmMx(a2+x2)3/2F = \frac{2GmMx}{(a^2 + x^2)^{3/2}}     * Asymptotic Behavior: When xx is very large (xax \gg a), the force is approximately:         FGm(2M)x2F \approx \frac{G m (2M)}{x^2}     * This shows that at a great distance, the system of masses acts like a single particle of mass 2M2M situated at the center of mass.
  • Example: Uniform Rod of Length 2a2a and Mass MM:     * A particle of mass mm is at distance bb from the center of the rod along the perpendicular bisector.     * Considering an element of the rod of length dxdx and mass M2adx\frac{M}{2a} dx, the force magnitude is calculated via integration:         F=aaGm(M2adx)x2+b2cos(θ)F = \int_{-a}^a \frac{Gm(\frac{M}{2a}dx)}{x^2 + b^2} \cos(\theta)     * Using trigonometric substitution x=btan(θ)x = b \tan(\theta), the result is:         F=GmMba2+b2F = \frac{GmM}{b \sqrt{a^2 + b^2}}     * As bb \rightarrow \infty, FGmMb2F \approx \frac{GmM}{b^2}, confirming the asymptotic point-mass behavior.
  • Example: Uniform Disk of Radius aa and Mass MM:     * A particle PP of mass mm is on the axis of the disk at distance bb from the center.     * Integration is performed over the area using polar coordinates (r,θ)(r, \theta), where the element of area is dA=rdrdθdA = r \, dr \, d\theta.     * Resultant force formula:         F=2GmMa2[1ba2+b2]F = \frac{2GmM}{a^2} \left[ 1 - \frac{b}{\sqrt{a^2 + b^2}} \right]

Gravitation by a Symmetric Sphere

  • Importance in Astronomy:     * The most important case for celestial mechanics and space travel is the spherical mass distribution.     * A "symmetric sphere" is defined as a body where the mass density ρ\rho depends only on the distance rr from the center: ρ=ρ(r)\rho = \rho(r).     * Newton proved that for a symmetric sphere of total mass MM, the gravitational force exerted on an external particle is exactly the same as if the entire mass MM were replaced by a point particle at the center of the sphere.
  • Practical Application (Earth):     * Earth's density is not uniform; it is approximately 3000kgm33000 \, kg \cdot m^{-3} near the surface but reaches 16500kgm316500 \, kg \cdot m^{-3} at the center.     * Because Newton's theorem accounts for varying density ρ(r)\rho(r), it remains valid for the Earth and Sun.
  • Proof Sketch (Spherical Polar Coordinates):     * The element of volume in spherical coordinates is dv=(dr)(rdθ)(rsinθdϕ)=r2sinθdrdθdϕdv = (dr)(r \, d\theta)(r \sin \theta \, d\phi) = r^2 \sin \theta \, dr \, d\theta \, d\phi.     * The total mass is calculated as M=ρdv=4π0aρ(r)r2drM = \int \rho \, dv = 4\pi \int_0^a \rho(r) r^2 \, dr.     * The total force magnitude is given by:         F=Gmρ(r)cos(α)R2dvF = G m \int \frac{\rho(r) \cos(\alpha)}{R^2} dv     * After complex integration using a change of variables from θ\theta to RR (where R2=r2+b22rbcosθR^2 = r^2 + b^2 - 2rb \cos \theta), the result simplifies to:         F=GmMb2F = \frac{GmM}{b^2}