00:01
Hello everyone as soon in the figure there is a uniform circular plate of radius 120 millimeter that is 0 .12 meter hinge at a and b to a clavis which rotate with constant angular velocity omega with vertical axis calculate first part angle beta that the plane formed with the horizontal for omega to be 15 radian per second.
00:58
Second part, omega max for the plane remains vertical.
01:23
Consider the centroidal axis x -dus -by -des -z -z -jad.
01:49
Sorry not centroidal axis.
01:52
Consider the axis see x -d -y -dase -s.
02:05
Suppose this is by -dess, this is x -des.
02:13
So this angle will be also beta.
02:18
Let us see here now.
02:20
Moment of inertia of the semicircular plate having the mass m, i x, dash, will be mr squared by 2, iy dash will be mr square by 2 and due to symmetry i x -y -dice, i -z -x -x -x -x -dase is 0.
03:14
Now angular momentum about the c at c we are finding i x does omega x dash i cap i y -dice omega y -d s d s i i x -d s i x is m r squared by 4 radius we are taking the symbol is smaller so here write smaller not capital r you may take that is your choice it is immaterialistic mr square by four radius we are taking the symbol by 4 omega sine of beta i -d s mr -square by 2 omega cos of veta z so we can write 1 by 4 mr square omega common then we can write minus sine of veta i -d s plus 2 cos of beta z say this is equation 1 angular velocity of reference frame c by dash z is omega which is minus omega sine of beta i -dus plus omega cos of beta z z so rate of change of angular momentum will be change of angular momentum rate of change of angular momentum in the reference frame c x -y -dase z plus omega cross angular momentum about c this term is 0 minus omega sine of veta i -d s plus omega cos of veta j -d s cross mr square by 4 into to omega minus sine of veta i -d -s plus cos of veta z -s.
08:06
Now simplify it, so it could be written as minus 1 by 4 m r square omega square sine of beta, cos of beta, k -caf...