M= O J= constant (also fori=1)conservation of angular momentum(1).Isolated systemFex=0Mex=0(2).Central forcerotation×Fex =0exPulsarNeutron starT = 1.187911second
Mex = 0 J = constant (also for i =1) conservation of angular momentum (1).Isolated system (2).Central force 0 ex Fi = 0 ex Mi = r Fex = 0 Pulsar rotation Neutron star T =1.187911second
Example<helicopter>① V-?How is the work down by F?Express F by J ,M, R3Solve:Rmv, = mvRRyRF11州y-1>0mymy222mv2J23FmR3R
<helicopter> Example : V=? How is the work down by F? Express F by J ,M, R. Solve: F 3 2 2 mR J R mv F = = R 0 mv 0 = mvR R R v v 0 0 = ( ) 1 0 2 1 2 1 2 1 2 0 0 2 2 0 2 − = − v R R mv mv m
Vellipse['FdR='dwRosunExamplej=rxmv=mvRk, =rxm,v, =myRkM =rxm g=-Rmgm,gm,gM, = rxm, g= Rmg
v sun ellipse = R w FdR dw R 0 0 m g m g 1 2 r r2 1 Example: → → → J = r m v = m v R k 1 1 1 1 1 1 → → → J = r m v = m v Rk 2 2 2 2 2 2 M r m g Rm g 1 = 1 1 = − 1 → → → M r m g Rm g 2 = 2 2 = 2 → → →
Problem 4-11kk1(r):Center force:V(r)福1L=×m=bmvkRVmOb0
Problem 4-11 Center force: o m b v R v = r r k f r 2 ( ) r k V (r) = L = r vm = bmv k0
k1I?mvomVb-212Yminbvo = rmin mVb一1bvo)?2+k一mom2-2km-mb=0mv1m22IminImin2k2b?=0Aminmy2k2k+ 4b2myomvoKk(k2+b2+mamn2m1>0(k+yk?+(bmy))minmvomn
min 2 min 2 0 0 ( ) 2 1 2 1 r k r bv mv = m + 2 0 2 0 2 min 2 min 2 mv0 r − k r −mb v = 0 2 2 2 0 2 min − − b = mv k r 2 2 2 0 2 0 2 2 2 0 2 0 min ( ) 2 ) 4 2 ( 2 b m v k m v k b m v k m v k r = + + = 0 r min ( ( ) ) 1 2 2 0 2 2 0 min k k bmv mv r = + + = = + b b bv r mv r k mv mv 0 min min 2 2 0 2 1 2 1