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Extra notes for circular motion: Circular motion : v keeps changing, maybe both speed and direction are changing changing. At least v direction is changing changing. Hence a≠0. Acceleration NEEDED to stay on circular orbit: acp=v2/r / , pointing i ti to t the th center t along l radius di direction. di ti Total force NEEDED in the radius direction to stay and maintain circular motion: Fneeded= macp=mv2/r , pointing to center 1. When total force in r direction pointing to center equals to mv2/r , it has what it needs to stay in orbit. orbit ΣFr = mv2/r , it stays in circular orbit. Neither flies away, nor falls into the center. Thi is This i how h you solve l related l t d forces. f V l iti or radius, Velocities di etc. t 1. Find ALL REAL Forces and force components, 2. ADD ALL in radius direction ΣFr, toward center. 3. Make ΣFr At that position equals to mv2/r at that position 1 4. Solve Equation ΣFr =mv2/r Chapter p 12 Gravity y Where does mg come from? Why is g=9.81m/s g=9 81m/s2 on earth surface? Sample problems: •What speed is needed to launch a object to fly around earth (close to earth surface)? •Where are the synchronous satellite (for TV) l located? t d? How to find the period of a planet orbiting around •How the Sun? 2 12-1 Newton’s Law of Universal Gravitation The force accelerating an apple downward is the same force that keeps the Moon in its orbit. Hence, Universal Gravitation. 3 12-1 Newton’s Law of Universal Gravitation The gravitational force is always attractive, and points along the line connecting the two masses centers: r is the distance between mass centers of m1 and m2 M 1m 2 M1 = G 2 ⋅ m2 Fg = G 2 r r 4 The two forces shown are an action-reaction pair. 12-1 Newton’s Law of Universal Gravitation G=6.67 x 10-11 Nm2/kg2, the universal gravitational constant G is a very small number; this means that the force of gravity is negligible unless there is a very large mass involved (such as the Earth). M 1m 2 M1 Fg = G = G 2 ⋅ m2 2 r r When m1 or m2 increases Fg increases. When r increases, Fg decreases. Fg is proportional to 1/r2 Att ti Attention: 1 over r square!! N Nott 1 over r. 5 When r is doubled, Fg will reduce to 1/4 of initial Fg. 12-2 Gravitational Attraction of Spherical Bodies Gravitational force between a point mass and a sphere: the force is the same as if all the mass of the sphere were concentrated at its center. 6 12-2 Gravitational Attraction between Earth and an object on it The center of the Earth is one Earth radius away from object m, so this is the distance we use: mM M Earth Fg = G = mg Earth 2 R Earth g Earth M Earth =G 2 R Earth M Earth = 5 .97 * 10 kg 24 Therefore, R Earth = 6 .37 * 10 6 m g Earth = 9 .81 m / s = 9 .81 N / kg 2 When m is on other planets Mp , Rp are different.7 g planet will be different from 9.8 m/s2 Example 1: Circular orbit around earth To let an object fly around the earth close to earth surface, you need to launch it with what velocity? In the radius direction, Force it has = what’s needed 2 v Fnet along l radius di = mg = m / r 2 v = g , so v2 = g.r gr r so v = so, g .r g in numbers: Plug Close to earth surface. g=9.81 m/s2 Earth radius r = 6370km = 6.37 x 106m V 7 V= 7.9 9 x 103(m/s) ( / ) ~ 5 mile/s il / Time to circle the world : T= 2 π r / v = 2 π 6.4 x 106 / 7.9 x103 = 5.1 x 103 (s) = 85 (min) 8 12-2 Gravitational Attraction of Spherical Bodies The acceleration of gravity decreases with altitude: 9 12-2 Gravitational Attraction of Spherical Bodies Once the altitude becomes comparable to the radius of the Earth, the decrease in the acceleration of gravity is much larger: Fg is i proportional ti l to t 1/r 1/ 2 10 Example 2, What is the distance h between synchronous satellite (for TV) and the earth surface? Synchronous satellite rotates around earth center t att th the same period i d as earth does, 24 hours. To keep circular orbit orbit, In the radius direction direction, The net Force the satellite has = what’s needed r = R Earth + h 24 hr = 86400 s 2π r / v = T = 86400 s v = 2π r / T GM m satellite v 2 satellite m satellite M Earth G = 2 r r M Earth G = v2 r 2 2 3 T = 4 π r Earth M Earth ( 2π r ) G = r T2 2 r=4.2E7 m, h=3.6E7m 11 Wow, all synchronous satellites are 36000km above earth surface. Example 3, How to find the period of a planet orbiting around the Sun? Assuming the orbit is a circle. Again, to keep circular orbit, in the radius direction, The net Force the planet has = what’s needed m Planet M SUN m Planet v 2 planet = G 2 r SuntoPlaen t rSuntoPlaen t G M SUN r = v 2 planet SuntoPlaen t v = 2πr / T 30 Mass of the sun =1.98892 × 10 T = 2πr / r kilograms You don’t need to memorize any results above. You only need to learn and solve ΣFr = Fg = mv2/r Use the correct r, correct mass and correct v. 12 Summary of Chapter 12 • Force of gravity between two point masses: • G is the universal gravitational constant: • In calculating gravitational forces, spherically symmetric bodies can be replaced by point masses. 13 Summary of Chapter 12 • Acceleration of gravity on earth : Combine gravity force with circular motion for orbits. Gravitational force = GmM/r2 = mv2/r •What speed is needed to launch a object to fly around earth (close to earth surface)? Know mg and r, r find v v. •Where are the synchronous satellite (for TV) located? Know T, Earth mass, G, find r ; (know v=2πr/T) v 2πr/T) •How to find the period of a planet orbiting around the Sun? Know Sun mass, G, r ; find v and T (know T=2πr/v) 14