Video summary
The video presents an intensive problem-solving session focused on gravitation concepts essential for JEE Advanced preparation, emphasizing the application of fundamental principles over rote memorization or extensive theoretical lectures. Students tackle a variety of complex scenarios, beginning with calculating satellite time periods by accounting for Earth's rotation through relative angular velocity and comparing revolution counts using Kepler's third law. The discussion extends to deriving exact expressions for orbits around different centers like the Sun versus a galaxy, analyzing equilibrium conditions on inclined planes with friction, and solving binary star systems where gravitational force provides centripetal acceleration based on center of mass constraints.
Further problems explore dynamic interactions such as dust clouds falling onto planets, requiring the conservation of angular momentum and energy to determine capture distances, alongside variable mass scenarios involving satellites accumulating drag that transition from circular to elliptical orbits. The session also addresses atmospheric pressure ratios by equating masses with constant density approximations and examines specific cases like rotating rods above Earth's surface where net centripetal force is calculated via integration over concentric shells. A detailed analysis of a particle moving through an Earth tunnel highlights the distinction between regions inside and outside, noting that angular momentum conservation applies only when external torque is zero, while energy methods are used to find maximum distances from launch points exceeding escape conditions.
The instructor clarifies two primary solution methodologies: utilizing force or torque versus conserving mechanical energy, explicitly stating that momentum conservation alone is insufficient without additional data regarding work done by forces like atmospheric drag. By relating changes in total mechanical energy to radial decay and velocity increases, the lesson demonstrates how kinetic and potential energies interconnect during orbital degradation. The session reinforces key concepts such as escape velocity relations and free-fall impact speeds while advising students to avoid unnecessary complications with advanced theorems when simpler fundamental principles suffice for solving intricate JEE Advanced questions.
In conclusion, the video underscores that success in this competitive exam relies on deep conceptual understanding rather than memorized formulas, urging learners to prioritize chemistry preparation alongside their physics studies to improve overall rankings. The final advice encourages students to focus on applying core ideas like angular momentum conservation when torque is absent and energy conservation where applicable, ensuring they can navigate both standard problems and the unique challenges presented in advanced gravitation questions without getting bogged down by superfluous mathematical complexity.
Read the full video transcript
Good day,
Hello everyone. Can you hear me? All of
you?
>> Yes sir.
>> Yes sir. Okay. Yes sir.
>> Should we wait for others?
Let's wait for 1 minute. Others will
join.
All
right.
Hello.
Fine. So, let us start today's session
on
problem solving of gravitation. Okay.
So we there will won't be any theory
discussion uh directly while discussing
the questions
there can be some relevant theory
discussion. Okay. So that is the idea
and uh I have taken questions
uh some of the questions are
which you might have seen before but
majority of them are little tricky in
nature. So if you are not able to solve
many of them doesn't matter okay because
I have ensured that many question you
should not be able to solve so that we
learn from this session okay so solve
this question.
You can DM your answers.
Okay. Shall we discuss now or should I
wait?
You can speak up. You don't need to be
on mute.
>> Yes, I think we can discuss this.
Okay.
See uh there is a satellite. Now the
satellite is not kept on earth. So
satellite's angular velocity can be
different from the earth's angular
velocity. So earth is also rotating. So
we need to account for that. All right.
So it is revolving in equatorial plane.
So earth also rotates like that wherein
this is the equator plane and earth
rotates like this and earth rotates
again from uh west to east direction.
All right. So uh the omega of the earth
is 2 pi by u we can write in hours omega
2 pi by 24 hours 2 pi by time period
right this is of the earth and omega of
the satellite
is uh 2 pi by 8 all right now we need to
basically see uh
with respect to earth Right? Because it
is observed vertically overhead a
longitude. So basically there's a person
standing on the earth who is observing
the satellite. Now that person is
rotating with the earth. So the person
is looking at the relative angular
velocity of the uh satellite. So the
relative angular velocity of the
satellite because you know if let us say
both the angular velocities are equal
then the person won't see the satellite
moving at all. It'll become like a
geostationary satellite. Okay. So that
is why relative anglo have to be seen.
So 2 by 8
minus 2 by 24
that you equate to 2 pi by time period.
Time period as in how much time it takes
to revolve. Right? So from here you'll
get the answer. Are we getting 12
everybody?
>> Yes sir.
Okay.
So you know one very important thing
that we sometime ignore is that the
earth is rotating. All right. So once in
a while that fact is used and time
period of rotation uh is 24 hours. So
omega you can easily find for the earth.
Do this.
Yeah, these initial questions everybody
should be getting it as a warm-up
exercise.
We can
I think many of you have already
answered.
Shall I wait for others? Anybody?
Okay. Now one very important relation
which is used so many times is t² is
proportional to r cube. Right? So uh
this is for the planet for the
satellite.
Yeah, somebody is saying something.
Okay. Right. So you know whenever
appropriate we should be using this law.
So t_sub_1 by ts2
because it's like the question is framed
in such a way that it's a comparison of
the time period of revolution
is equal to uh r / 4r
cq right so t_1 by t2 is uh 1 by8
right
4 is 2 square. So square square get
cancel 2 cube. So 1x 8. So time period
of this satellite B if it is 8 hours
then for A it is 1 hour. That way you
can think. Now in 1/4 year 1 quarter
year is 8 / 4 it becomes 2 hours. How
many revolution A will make? 1 hour it
makes one full revolution. So in 2 hour
it'll make two full revolutions. So
answer is two.
Okay. So you may have your own way of
reasoning it but this is how you do it.
Okay. Any doubts anybody?
Nothing.
No doubts.
>> Okay.
Good.
One more.
There's also a
straightforward question.
Do it.
If you do gravitation properly then
you know electrostatics, laws of motion,
work by energy many chapters
automatically are getting you know
revised. So don't think that it is only
gravitation you are studying. Soon
you'll realize that many concepts from
different chapters are utilized.
Only one person has answered till now.
What else?
Okay,
three,
four, four people have answered and all
four of you got it correct. That's good
to see.
I'll do it.
All right. See, uh it is somewhat
similar to the previous question. But in
previous question,
if you see
uh both the planets are revolving around
the same center point which is sun.
Okay. But here
uh the sun orbits sun is orbiting and uh
the earth is orbiting sun. So basically
there are two center points of
revolution. So you cannot use t² is
proportional to r cube like that here
because there two different scenarios.
But uh you know there is an expression
between because you can see the options
also and the question is framed in such
a way that it is about time period and
the uh radius of the revolution. So
we need to basically get the exact
expression wherein
yeah wherein there is an in uh there is
an equal to sign because we can't use
proportional to because proportionality
constant for both the scenarios will be
different as there one is revolving
around Milky Way and one is revolving
around the sun. So I mean do do you guys
remember that exact expression or not
or you tend to derive it
>> the time period one for orbit?
>> Uh t² is equal to what into r
>> I derived it.
>> You derived it. Okay. Yeah even I would
have derived it. I don't even remember
people's name. Forget about the
formulas. So this is the
m instead of v square I'll use omega² m
omega square r right so m and m get
cancelled so um um what
you can say omega² is equal to in fact
>> 4 pi square by t² right
>> uh thank you so this is 4 pi² square t²
r. So then it becomes r cq is equal to g
m by 4² t². Right? So this is where
you know this m is coming.
So in the first sentence where it is
revolving on the galaxy
uh this is the mass of the galaxy and
this is capital t and this is capital r.
And in the second situation instead of
capital R it is small R and this is mass
of the sun now
and this is small T².
So you know since there is an equal to
sign you you don't need to assume that
proportionality constant should be
equal. So now you can divide it and get
a ratio of mass of galaxy with mass of
sun.
Okay. In both the scenarios we are using
t² and r cube relation only but here you
can use just proportionality
and divide so that constant get
cancelled but here they're two different
revolutions so proportionality constants
are not same so you need to get an equal
to sign so this is how you solve it and
probably a is the answer because
majority of you have said that not 100%
sure but this is how you do it okay
shall I go forward
Yes sir.
>> Okay. Now get ready. We'll just uh go
one level up.
Okay. And do it uh maybe uh you should
be very very I can say honest and if
you're not getting you're not getting at
least you'll learn something but if you
get the answer from somewhere somehow
then you'll not learn also. Okay. So
just focus on the learning. Do this.
Um just draw the free body diagram
show the forces and the horizontal force
should be
less than or equal to mu time normal
reaction.
That's all you have to use.
Grav intensity of gravitational field is
nothing but acceleration due to gravity.
Force divided by mass is accession to
gravity only that is intensity.
I'll do it.
One second.
Yes, I can do.
Okay, some of you got some answer.
Okay,
let's do it then.
So assume that this angle is theta.
Okay, let me take it horizontal only
like that.
Yeah, this angle is theta. So there is a
this B is here.
It is evolving
B is here. Okay. So this is the
gravitational force
between this mass and B which is mass
capital M. Then
it has mg over here.
It has normal reaction.
Okay. And uh
you can assume a plane which passes
through all these forces
and this is your friction force.
Do you all understand the I mean any
doubts in free body diagram?
>> No sir.
Nothing.
>> Nothing. Okay. Now uh
you have uh vertically you can say n +
fg sin theta minus mg is equal to zero.
Right? So n is equal to mg minus
gravitational force
sin theta.
And uh friction force should be um
less than or equal to
mu * normal reaction right
and uh
horizontally this is the normal force
horizontally there is
uh
I can write like this f minus
fg G cos theta is horizontal
right this should be uh
equal to zero.
So friction force should be equal to fg
cos theta and friction force is
this fg cos theta
should be uh
less than or equal to mu time normal
reaction. So m g minus f_sg cos theta.
So sin theta sir
>> sin theta sorry
sin theta
is this fine till now
the range of
>> yes sir I reached this equation too I
didn't know what to do after this
>> between so that you remains motionless
okay so what is the value of FG. FG
is g mm
by R².
G mm
by R² cos theta
less than equal to mu mg
plus
this.
So we need to basically see theta is a
variable we need to get rid of it.
Now
so value of theta is there in the
diagram
>> what
>> the by 2 minus theta we can write
it as sine of by 2 - theta is
>> no no no
anything is missing here friction is
equal to fg cos theta Uh
>> no sorry I got the same equation
>> I tried making it as an equation in
terms of mu and then finding its like
minimum value or something so that mu
can be greater than that
>> but that didn't work.
>> It should work.
>> The derivative is very weird.
>> You don't need to take derivative
everywhere. Keep quiet one second.
This now we need to get rid of theta. So
see theta is a variable. So can anybody
tell me what is the maximum value of
this? What is the maximum value of this
>> under root 1 + mu square?
>> Under root 1 + mu square. So the maximum
value of this should be less than mu mg.
All of you agree or not?
Huh?
>> Yeah.
So g mm by r² maximum value is 1 + mu²
should be less than or equal to mu mg
and when I'm gone so this will get you
the value of mu is it clear now
>> yes sir
>> has anybody done like this anyone
Okay.
All right.
Fine. So, uh, as far as I know, the
answer is C.
If you simplify, you should get C. Let
me check. Final answer
C. Final answer is C. Correct.
Okay, shall I move ahead? See, this is
where you know I have seen many Olympiad
questions in which they get something
like this you know cos theta plus some
constant time sin theta and you have to
take the maximum value of that. So that
that that is how it it should click to
you as well. Okay, it's not that you can
substitute the value of theta to be
something. Uh basically you can use
calculus or whatever you want to because
this is the only thing that is changing.
So you need to maximize this.
You can maximize using trigonometry as
well.
Fine. Shall I go to next?
Anybody has any doubts?
Any doubts? Anybody?
Okay.
Go to next. This one.
You need to think freely. Then only you
will be able to these able to do these
kind of stuffs. You can type in your
final answer. I I'm giving you maybe
four or five minutes. I should not
disturb you. So four five minutes I'm
giving
Collinear
means that u they are all rotating
together like a stick. Consider a
straight line and uh entire the entire
straight line is rotating.
Okay. And uh the both the stars and
ships are on that straight line.
Uh checking whether orbit is stable or
not is beyond our scope.
So ignore the second statement. Actually
it is not stable.
Shall we?
I hope uh some of you are in middle of
thing.
Any
physics question, any question
starts with a diagram.
A proper well-labelled diagram is half
the question done.
Should I write the final answer? Final
answer
I have
m1 by m_sub_2
R2.
This is the final answer.
Anybody
fighting still to get the answer?
About 2 minutes.
So you got the answer got some answer.
>> No sir.
>> Van
>> no sir.
>> What is stopping you?
You don't know from where to start. Is
that the issue?
>> No, I kind of did find a place to start.
The the entire system if it's coina
would have the same angular velocity
about some point, right?
>> What is that point?
>> I tried to find that point. That's what
I'm not getting.
>> Are you sure? I mean can anybody help?
What is what could be that point about
which uh entire thing is rotating? What
do you think? Pune. I'm in a class. So
probably the center of mass the binary
star system.
>> Exactly center of mass.
So everything you look at with respect
to center of mass that is a good
starting point. And then
haven't I told you uh in 11th and 12th
that if anything is rotating in a circle
what equation you should write first?
What is that first equation? Enter
your first one.
>> Anything rotating in a circle, you have
to write force toward the center is m
omega² into radius. That is the first
equation you should write. And that's
all you have to do in this question.
And what is that center? Center for all
three is what?
center of mass.
Should I do it now? We just write the
equations.
A can can you do one thing? Draw the
diagram. All of you represent all these
values
and then uh I will just write down the
equations. Do it quick.
>> You have a doubt in the diagram.
diagram.
Let me let also draw the diagram and
then we'll discuss right now. What do
you understand? Draw it.
Okay. So, I hope all of you have drawn
it. So, this is that line.
This is one star. This is the other
star.
One is m_sub_1 and m_sub_2. Now there is
a uh spaceship also. Now spaceship mass
is so little compared to star that we
can assume center of mass doesn't shift
anywhere. So center of mass is let's say
here. This is our center of mass.
Okay. Distance spaceship from the star
is R1 and R2. So this is your R1.
This is your R2.
But the revolution is happening uh with
from know
uh the center is center of mass. So R1
and R2 they are not the distance from
center of mass. So you need to assume
something. So you can say this is a
this is b
you can say c also but you don't need
distance of center mass from uh the uh
spaceship because that you can get now b
minus r1 that is okay so yeah tell me
what is the issue with the diagram
>> sir how are you so sure that the
spaceship has to be between the stars
and not some place
How? What?
>> Like why does it have to be between the
stars?
>> That is the condition. They are
colinear.
>> But they can be collinear if the
spaceship is not in between the stars
also.
>> How it can be colinear? If it is here,
how will you make a straight line
connecting?
>> On the same line, but on one of the
sides on the same side.
>> Okay. Okay. Okay. Yeah.
>> But then it wouldn't be much of a
spaceship, would it? If it can't see one
of the stars.
>> No, no. Let it be that side also. Let it
be. It doesn't matter. Uh if you if you
keep it here, okay, and then rotate it
that is also fine. But then you know
since in the question it is not
specified whether the spaceship is in
between or outside. So clearly it
doesn't matter.
But then you have to solve and if you
have to solve then you have to assume
one of the two scenarios and whatever
scenario you assume the answer should
come out to be same
right so you can't get confused for that
because it doesn't depend on it since it
is not given is it clear Arita
>> uh yes sir
>> so I I hope you understand how it is
revolving everybody this binary star
revolves around center of mass like
this.
Okay. Whereas this m1
can revolve about center of mass in a
bigger circle like this. So both of them
are revolving around the center of mass
as a center.
Now I have to erase this.
>> Excuse me sir.
Um I thought why can't the satellite be
at the center of mass itself
that becomes a specific scenario that is
not a uh you can
keep it answer won't change still
>> okay
>> but I try to solve like this okay fine
uh
if the spaceship is at the center of
mass then then it is always colinear
isn't it? it'll be always colinear then
uh whatever is a value of m1 and m2 it
will be colinear only because androath
doesn't move and if what goes like this
and m1 is here m2 is there yeah it'll be
always colinear
anyways let's solve for this scenario so
first of all um for this center of mass
for this to be center of mass
All of you agree that moment of masses
should be equal
this equation. All of you
know this or not?
>> Yes.
>> Yes sir.
>> Okay. Then the constraint relation A + B
should be equal to R1 + R2.
This is second. So using these two you
can get either A or B in terms of R1 and
R2. Right? So that is one. Then u let us
say angular velocity is omega.
This is omega. This is omega. So the
force on m_sub_2. What is the force on
m_sub_2?
G
m_sub_1 m_sub_2 divided by r1 + r2².
This is the force toward the center of
mass. Right? I hope all of you agree.
I'm ignoring the gravitational pull by
the spaceship on the star. Is it
negligible? This should be equal to
m_sub_2
omega² into what? What should I write
anyone?
>> Sir, you're doing this for m2, right?
So, it's distance from the center of
mass.
>> So, what is that? That is what I
>> a
now somebody will somebody else will
answer the next one. So for the m1 we
can write g m_sub_1 m_sub_2 by
see for m1 we should not write because
it becomes a redundant equation. You can
see here if you write for m1
it'll become like this m1 omega² b
right? So if you combine three and four
it becomes one. So it gives you
redundant equation. Equate right hand
side of three and four it becomes
redundant. So we don't write redundant
equation unnecessarily.
But now we will write the equation for
the spaceship.
Can you all write that equation? All of
you please write.
Let me know once you're done.
Done.
Others are you guys done
for the spaceship?
Spaceship is getting pulled this way and
this way. So towards the center of mass
force you have to take that is g
m_sub_2 m is a mass of spaceship divided
by
what is the distance r2²
minus
g m_sub_1
m by r1² this should be equal to m
omega²
distance from the center of mass is
What?
For the spaceship, what should I write
here?
>> B - R1.
B minus R1.
I told you let somebody else tell.
Anyways,
so these are the four equations. You
have to play with them and get the
answer. M1id M2. Okay. So
mathematically it appears that it is not
an easy equation to solve but you know I
think you should be able to the these
three and four you uh there is b and a
right so you can write a as r1 + r2
minus b here and then substitute b as uh
you can get b in terms of r1 and r2 by
writing
uh
this a as m_sub_1 by m_sub_2 * b is b is
equal to r1 + r2. So you can get B in
terms of R1 R2. Substitute here. A you
write R1 + R2 minus B. Substitute here
also. And then just play with it. You
get the answer. Okay. I'll move on to
the next question.
Right. Okay.
Are you finding it tough?
>> Interesting is a better word, sir.
What
I
>> mean it's more interesting than just
tough.
>> Okay. Should I give you mo much more
interesting ones? Everybody
>> I don't think so. Sir, I think this is
enough for today.
>> I have these kinds
do this.
I'm giving you another five minutes to
solve.
What is that first thought that comes in
mind when you read this question in
order how to solve it? First step
>> may
>> uh B
>> escape velocity will be different for
every particle depending on how far away
from the planet it is. Correct.
>> So you're just taking the escape
velocity clue from here and trying to
fit in how do I solve with respect to
escape velocity using that as a starting
point. Basically I'm trying to find the
that distance from the planet below
which every particle gets captured into
orbit.
>> That velocity below which every particle
get captured.
>> That distance from the planet because
all of them have the same velocity.
>> Uhhuh.
>> There will be some distance from the
planet. I said velocity will be
sufficient to escape orbit completely
and leave the planet not get captured.
Anything below that will get captured.
So if I can find that value of r then
that gives me the thickness. I already
have the length and density.
>> Great. So is saying what Van is saying
that this is the cloud. Uh right this is
the cloud. So he's trying to find out
how far the particle can be in order for
it to get captured by the planet. Right?
That's what you're saying. So how will
you basically get that how far it is?
What is that limiting condition for
which it should get captured?
You understand my question?
>> Yes sir.
>> How do you get that this is the farthest
away the particle will be for it to get
captured with the planet?
So should the velocity in the direction
of the planet be greater than the escape
velocity?
Velocity in the direction of the planet
as a component this component.
>> Yes.
>> It is coming towards the planet. Right?
So whether it is greater or not it will
fall on the planet. It's not going away.
If it is going away then escape velocity
comes in picture.
Think more.
>> The point at which escape velocity
becomes zero of a particle.
>> Escape velocity becomes zero is
infinite.
So that is like entire cloud will get
captured. in
don't get fixated on escape velocity
that is what I would say because
particles are moving towards the planet
it's not that it is going away
I mean
I know even I when I was solving before
the session I was uh reading too much on
this SK velocity thing but it's not
about SK velocity it is about something
else
how the
>> about conserving momentum
>> how the particles
will come towards the planet how do you
think they will travel they will get
attracted by the gravitational pull
right oh
so these
two straight away get into like this
suppose this particle how this particle
will go to the planet it travels like
this and falls like that
isn't it it falls like that
now can I say can I say that all the
particles falling on the planet has the
same velocity
is it true or not
>> yes sir
>> you can conserve energy and you can see
that initially they are moving with what
velocity vot
and kindic plus potential is constant.
So you know that uh just before reaching
the planet every particle's velocity
will be equal.
So it's not about uh that some particle
will have a different velocity compared
to other but still some particles will
miss the planet.
Why? Why they will miss the planet?
Because they will go like this instead
of falling on the planet.
they will get attracted by the planet.
So that is why they get deviated but it
doesn't fall on the planet. Just imagine
a particle is just falling on the
planet. Then what will happen to the
particle? Particle go like this and
tangentially touches the planet like
this. Do you all agree?
Not getting it.
If let us say this is the planet. Okay.
This is the planet.
So
this particle
the limiting case the particle will
travel like this
and will just go tangentially like this
and falls on the planet. Do you all
agree? The particle just
>> just above the particle will miss the
planet. It'll go like this.
>> Agree? All of you? Can you type in or
speak?
>> Yes sir.
>> Right. So the limiting condition is that
what is that condition? That the
particle when it reaches the planet its
velocity is tangential.
That is the limiting condition.
Now can anybody guess what could be that
uh physical concept we should be using
to capture how far the particle should
be from here? What law can we use for
that situation? Because this distance
like what Van said if you get this
distance then I can just imagine a
circular cross-section here then all the
particles have the same scenario and I
need to just get volume of the cylinder
multiply with the the density I'll get
the answer right. So how to connect this
velocity, this distance and this
velocity
and some distance.
Which concept?
>> Projectile motion
>> which law
>> we can conserve angular momentum.
>> Angular momentum. You have to conserve
angle moment about what? About this
point. About this point the particle is
experiencing no torque. Isn't it? Only
this planet is applying gravitational
pull this way. This way all the pull is
passing through the center. So if you
can conserve the angular momentum about
this point, you can connect the initial
point and final point.
That is how you have to connect, right?
You you know this you know some of the
initial condition you know its velocity
you know some of the things about the
final condition. So if you connect them
you get an equation and to connect them
you have to use conservation of angular
momentum. Is it clear making sense to
everybody?
Speak up. Is it clear?
>> Yes, sir.
>> Yes.
Who else has to say?
Okay.
>> Yes.
>> Yes. Okay. Fine.
So,
should I do it or you want to do it?
You do it. Get the equations. Complete.
Don't you don't need to solve it. Get
the equation which will be used to solve
and let me know once you're done.
type in once you're done writing the
equations.
You have to write three equations
conservation of angular momentum I'll
write mass of the particle let's say mp
mp v into d
angular momentum about this point. How
will you get get the perpendicular
distance
perpendicular to velocity the distance
is d. So this should be equal to mass of
the particle
v into radius of the planet is r. What
happened?
V into r v into r.
So v into r should be equal to v into d.
That is the first equation.
Then you have uh conservation of energy
half mass of the particle
v²
minus g
um
is it very far in from dust particular
planet from great distance. So potential
energy initially is zero.
This should be equal to half
mass of the particle into v² minus of g
mp
by r.
Now mass of the planet is not given but
escape velocity is given.
That is where they want you to use that
stuff. So you know that escape velocity
is roo of 2 g m by
r isn't it? So gm by r becomes uh sk
velocity squar divid by 2. So this is sk
velocity squar divid by two. This is the
second this is the third.
Then you have to basically find
mass. How much mass of dust particle has
been collected?
Collected mass once you get the value of
d is pi d² into l.
This is the answer.
Okay.
Any doubts? Anybody? You can speak up.
Final answer I don't have for this
but I I hope you got the questions right
T.
Okay.
All right. Shall we move ahead?
>> Yes.
>> Ready.
5 minutes for this.
Yeah, rod has mass, bead has mass.
Look at the distances carefully.
Rot and L and X.
R is extremely large.
Did I do it?
Okay. So let us discuss this one.
So uh
prana how will you do this? How will you
start? What is the thought process?
Maybe because the
force there's there's a very very tiny
difference in distance across the rod.
So maybe that would affect the
acceleration of the rod compared to the
bead. And we try to figure that out.
>> That will affect what
the relative acceleration of the bead
and the rod.
So you're basically trying to find
relative acceleration of bead and the
rod.
H
>> that's what you're trying to good that
is what you have to do find out the
accation of the rod find out the
accation of the bead and then get the
relative acceleration
okay because they're asking how much
time it takes for the bead to come out
right
uh so bead is moving on the rod so broad
is also moving so to get the relative
acceleration
for that I need to have I need to get
the force
on the rod. So to get force on the rod
you have to consider at a distance of x
dx
thickness of the rod mass per needle
length lambda. So the df force is
g mass of the earth into lambda dx mass
of the small mass of that into divided
by x²
right this is a df
integrate this
you'll get the value of force on the rod
right and force on the rod should be
equal mass which is lambda into L time
accation of the rod.
So from here you'll get acceleration of
the rod.
That is clear right? This will give you
accation of the rod. Now acceleration
there is an approximation probably
involved here. So let me do it
completely.
So,
g m lambda
um it goes from r to r + l.
So 1x r - 1x r + l. So I'm assuming the
force on the rod to be constant. Is it
true that it is constant?
Because r can keep changing. Yes or no?
>> Yeah. Yeah. So it'll vary as it gets
it'll increase as it gets closer, right?
>> Huh? So but why I'm assuming it to be
constant?
>> Because r not is much much larger.
>> Rot is extremely large and we are
talking about the time in which the bead
will come out. That time would be in
seconds or minutes or in hours let us
say. But this 4 into 10^ 8 m nothing
will happen to it. So that is why we are
ignoring the variation of the force
between that time interval when the beat
comes out.
So this is G M R L / R + L.
This is expression of the rod. Now
acceleration of the beat.
Acceleration of the bead is u
a force we can write directly g m is a
mass of the bead let us say divided by r
+ x²
this should be equal to m into accation
of the bead.
So accation of the beat
is g m /
r + x².
Now x note is very small compared to r.
So you ignore x from here. So it will be
g m / r². So this accation of the beat,
right? I'm adding x not to r. It doesn't
matter.
So the relative acceleration is
acceleration of the bead minus
acceleration of the rod. This is your
relative acceleration.
And once you get relative acceleration,
you know x not is equal to half a
relative t². So from here you get the
value of t.
Clear to all of you? So in this question
you have to think in a very simple
manner and use approximation to get the
answer. And you need to appreciate the
distances involved. If you don't
acknowledge the fact that distances are
very small compared to R not, you'll
make it extremely complicated. And some
of you might have done that.
Right?
All of you clear about this? Shall we?
Okay. 5 minutes for that this one.
Okay. So we will discuss.
Okay. One answer
to two people got the answer.
Who will uh explain the thought process?
Any
what do you think how will you how will
you proceed?
So first I try to draw the diagram
diagram. It is found or it has
atmosphere right
diagram 10 then
Hello.
>> Am I audible? Any
>> Oh yes sir. I was uh on mute.
>> After that I tried to uh like
>> I tried to like understand the situation
and like write some equations. I wrote
the equation with uh
I wrote the equation of the force uh I
took like a small volume in the
atmosphere.
>> Okay. So you you you use a small volume
to do what? How will that help you?
It
gave me like a proper mass and object
point object so that I could write my
equations easily.
>> What equations? That's what I'm asking.
What are you trying to write? What are
you trying to achieve using?
>> I wrote the equation of force using
>> force. Correct. So you are writing force
equation so that you get accession due
to gravity.
>> Yeah. As to gravity is total
gravitational force divided by mass.
>> Yeah.
>> So you're trying to find force on that
imaginary point mass kept at a distance
of x away. All right. Now the force can
you divide into two parts? One from the
planet and one from the uh this thing
atmosphere.
Right? Now what you can say see for the
planet it is straightforward right? The
force from the planet
you can directly write g mass of the
planet into mass of the particle divid
by x². But how will you consider the uh
force due to the
atmosphere? How will you take care of
that?
Should I ask somebody else?
Okay, I have troubled you enough.
>> So, is it only because of the inner part
of the atmosphere and not the outer?
>> So, you can draw one imaginary spherical
shell
and you know the shell theorem only the
mass that is within this green sphere
can apply the force
and it'll apply the force as if it is
located at the center. So you just need
to find how much is this mass and
whatever mass comes here you can direct
write g into m uh gmm by x²
that's all. So mass of this atmosphere
which will apply the force
mass of the atmosphere again you you all
know you have done it enough number of
times 4 pi r²
d r row into dv right integral
so 4 pi row integral of r² d r integral
will go from where to There
>> so row is not constant right
>> sorry sorry sorry 4 pi integral row is
sigma by r so 1 by r r² d r so limit
will be from where to where
>> to x
>> from so r to x - r
>> r
X
right so it'll become 4 pi pro
becomes X²
-
R² by 2.
So this will become mass of the
atmosphere. So the force
total force is
g mm by x²
plus g mass of the atmosphere which is
2i sigma
x² - r² m divided by x²
now gravity g is f by m. So m and m
gone.
So you can write this as g m by
x²
-
2 g
sigma
by x² into r² this I'll keep it separate
plus 2 pi sigma
g. Now this G should be independent of X
because it is said that it should be
constant throughout. It'll be
independent of X only when this bracket
term is zero. So equate it to zero.
Then it becomes G becomes constant which
is this
clear to all of you.
Speak up guys. Is it clear?
Yes sir.
>> Okay.
>> Yes sir. Clear. Final answer comes out
to be
final answer.
Someone got the answer. Wait m / 2 pi r.
Oh that is your answer only. Same answer
also got.
>> Okay. All right.
Only the part one 5 minutes for There.
Okay. So shall we discuss?
What does Huns
Say
>> okay
from Vipure is it?
>> Yes.
>> Okay. Okay.
All right. So
who will T?
>> Yes sir.
>> Tell how to start.
Um, atmospheric pressure is the total
force applied on the earth by the
atmosphere divided by the area of the
earth.
>> Mhm.
>> And we can find the force applied by the
atmosphere on the new planet by the
gravitational force.
>> But what is
you're trying to achieve ratio of
atmospheric pressure on the surface of
the planet to the earth. So given
whatever are the scenario whatever
whatever parameters are given here uh
mean density mass mean density why why
do you think mean density is given
>> uh like average density so you don't
have to you just multiply it with the
volume
>> exactly right diameter of the planet is
given its mean density mass of the
atmosphere dor not and I'm not
okay. Mean density of the atmosphere is
same. So atmosphere's density is same.
Now suppose atmosphere density is given
and the height of the atmosphere is
given.
What could be the atmospheric pressure?
Then
>> uh you would need to integrate for
different points cuz the gravitational
force
>> you're assuming density to be constant
mean density of atmosphere. So
>> and then you have to multiply with the
volume of the atmosphere as well to find
the total mass of the atmosphere.
>> Are you sure?
Mean density is given. So I can just use
ro gh
yeah we can do that as well.
>> I can directly I don't need to integrate
that is why you know the mean values are
given here. So if let us say I have to
solve the first question it should be
like uh
uh mean density
of the atmosphere
is same right so let's say that is sigma
kn sigma kn g sigma kn g1 h1
divided by sigma g2 h2. So the answer
should be G1 H1 divided by G2 H2. I do
not know the value of G1 H1 and H2. So
this is now I will try to find out G1 H1
and G2 H2. All of you agree everyone
this is Earth.
This is planet.
Okay.
Now how will you get H1 and H2? What do
you think everyone
>> of the atmosphere?
>> What?
>> They give us the mass of the atmosphere.
>> Huh? So how will you do that? It is the
mass of the atmosphere of the planet is
10 times the mass of atmosphere of the
earth. So how will you use that
>> volume? because density is constant.
>> H. So what should be the equation? What
should I write?
>> So it's given that height of atmosphere
is very small compared to radius.
>> So instead of using the volume of a cube
thingy volume of a sorry sphere, you can
just take surface area into height.
>> What should I write here? So surface
area will be 4 into r² or p
into d² where d is the diameter of the
planet
time h is height of the atmosphere will
be equal to the volume of the atmosphere
>> and mass by volume is constant for both
planets
fine so you can do that and you can
equate the uh
so let's try to do that so m not is
basically what you are saying is 4 pi
radius of the earth.
You have to write 4 pi r²
into this is h2
that into uh density of the
atmosphere sigma knot.
Now
the 10 m should be equal to 4 pi radius
of the planet²
time h1 into sigma kn.
Are you able to understand everybody
this equation what I'm writing here
this is m not right? So I'm writing 10 m
as 10 into that. So this equation all of
you get this equation
you type in
I mean you don't need to do this
approximation what you could could have
done is uh sigma kn into 43
4 by 3 into
r
earth + H
2²
H2 cq minus
R earth cube and then use binomial
approximation you get the same thing
because h is very small compared to so
you can use binary approximation take
outside okay can you type in is this
equation clear or not
everybody Ready? Is this equation clear?
Okay fine. So radius of planet is how
much time of radius of earth? 10 times.
So we'll get something here.
So we'll get 100
into h1
should be equal to 10 into h2.
So h2 is 10 * h1.
that is you get h1 by h2. Now g1 by g2
that is I guess easier
uh diameter mean density is this. So
basically you need to get the value of g
in terms of density
this is g m divided by
r².
So m is 4x3
r cq into density
divided by r².
The small g is 4 g
r row by 3. So g1 is this g1 is for the
planet.
uh density is
4 g by3 radius is 10 * radius of
the earth
and the density is
row node by 4 so 10 x4 is 5x2
so 5x2 * of g2
g1
right so we have g1 G1 by G2
5x2
H1 by H2
1x 10.
So multiply
uh multiply so you'll get 1x4
that should be the answer
clear to everybody.
This is not Olympiad. Okay. This is I
think one of those J advanced questions
only. The last two three questions were
not olympiad.
Is it clear to everybody
type in anybody has any doubts you can
speak up.
No doubts nothing.
I'll move ahead. Okay.
Five minutes for this. You'll do both
parts
take six to seven minutes. both parts.
Anyone?
About to get anyone about to get the
answer?
Okay.
How to proceed? Sumat
is there?
You're on mute. Samar
is not there.
Okay. Shorty, how will you do this?
>> So for this question, we are talking
about a satellite which is pretty close
to earth and now we are saying that this
collides Indian accent. Then exit.
>> So sir, we are saying that there is a
satellite that is hovering over the
earth and there's a cloud of dust
particles that comes into contact with
this particular satellite.
>> So because of this uh it appears that it
experiences it experiences some kind of
a resistive force which decreases its
velocity. And we know that since this is
going in a circular orbit, omega cannot
change. So if velocity decreases, then
something else must make up for it.
Meaning the radius also decreases and we
proceed from there.
>> How will you find force?
>> So I did dm by dt into velocity.
>> Right? So you might have seen some
scenario where you must have encountered
some question with bullets are hitting
the wall and you have to find the force
or uh or you might have seen scenario
where photons are hitting the surface
and you need to find the force. So there
rate of change of momentum is what you
need to find. So um and
in case of fluids also you might have
seen force
we have to here mass is changing right
as it keeps sticking on it mass is
changing so force is v dm by dt force is
m dv by dt plus v dm by dt also okay now
velocity is changing very very slowly so
we are ignoring that so it is just
simply v dm by dt
I hope this is clear to everybody.
>> Yes sir.
>> Uh don't count.
>> So I have a doubt here.
>> H
>> uh we said that velocity is changing
very slowly but it's still changing
right. So do we have to write it as a
function of mass over here or we just uh
assume that it's the same velocity
throughout?
We're assuming it is same. I mean it's
it's that uh variable mass scenario. So
we are ignoring that change in velocity
extremely less
>> sir. But can't we find that velocity if
we uh conserve momentum?
>> You can do you can do why not? You can
do all that. But you're not supposed to
do. We need to all understand that what
you supposed to do what you're not
supposed to do.
So sometimes we are running behind
highly accurate scenario mathematically
unnecessarily. For example, here the
mean radius is given. So simply we have
to write row GH. But the first thought
that comes in our mind to integrate then
uh what else there was this scenario
also here we ignored x not compared to r
not so physics is not about being 100%
accurate because
u
you know if you complicate it
and try to include everything probably
you will not be able to solve the
equation itself.
Okay, but then we'll talk about change
in velocity in the second part. Anyways,
it changes but it changes extremely
small rate. So, we are ignoring that.
Fourth is V DM by DT and
DM is what?
It is area of cross-section S
dx
is dv dt into row. So it is row s v² s
is a cross-section area which so
basically as it is moving
the dust is sticking on it and rate at
which dust is sticking
that is what is dm by dt
okay so this is the force now how will
you find the velocity with what velocity
it sticks
how you get
it's The orbital velocity don't you
think so? So it'll be g m by radius of
the earth² that should be equal to m v²
by r. So v² is equal to g m by radius of
the earth
that will go there and you'll get the
value of force. This is your first part.
Okay. And it is no longer moving in a
circle. Its radius
shifts continuously.
And if dust is there, it will slowly
falling into the
falling in here. Right? So basically you
can't even use this equation. You can
argue that how can you use this
equation? This equation is valid only
for the circular motion. But it is not
perfectly circular.
So how will you get the second? How will
you solve second part? Any ideas?
Anybody? Anybody wants to
tell?
Second part. How will you do it?
So since torque is torque is zero about
all the center. Do we conserve the
angular momentum and try to find the new
radius?
Find the change of velocity and the
radius of the server path.
But to find the new radius you need to
know the new velocity. Isn't it?
And do you think angular momentum is
conserved?
Are you sure? Isn't just creating that
external torque with respect to center?
>> Can we conserve linear momentum in the
collision?
>> There is a force. The force is only you
found drag force is there.
Right? So if there is an external force,
think more. Think more how you find
change in velocity.
So can you find acceleration like the
tangential acceleration using the
>> using this you find the tangential
acceleration
>> this is the force this force equal to
mass into tangential then what
>> so and they've said that it's one
revolution so you know the time period
for one revolution anyways
Yes, you can that you can do that ways.
Any other way can think of anyone
see there are only two ways to handle
either you use the force or torque or
you use the energy. Okay. So in
conjunction to the momentum
conservation, momentum conservation
cannot completely solve your question
until unless something is already given
to you. So either in mechanics you'll be
using force or energy. So there are
always two ways of solving question. You
can use energy. But in order to use work
energy theorem you have to use work done
is equal to change in the
uh total energy. Right? Now why I'm
putting negative total energy work done
over here is it positive work done or
negative work done in one revolution
when it is revolving
>> negative it
>> is negative so work done is minus of row
s v² now here also approximation I'm
assuming this force to be unchanged in
one revolution but the fact is slowly
the force is you know decreasing uh as
it is uh going in sorry it is increasing
because velocity has to probably
increase as its radius is decreasing. So
but then we need to keep that uh
approximation and this is
this one and uh total energy of a
satellite is what? Do you remember minus
of G mm by 2R? Do you remember this kind
energy plus potential energy is this?
>> Yes sir.
>> Right. So this is equal to uh
change in the energy. Now this is E. So
delta E is
G mm
by 2 R² into delta R
because delta R is very small I can use
derivative concept here. So G mm
by 2R² delta R this will give you delta
R. Delta R is negative because it is
coming in. So delta R is negative.
>> So won't delta E be caused by change in
velocity also.
>> Yes, it does. Velocity is a function of
R. Velocity is a function of R. So this
is kindinetic energy plus potential
energy sum of both.
>> Okay. So
>> see uh let me complete. See this is the
delta E. Once you know delta E let's say
you got the value of delta R using this.
What you can do next is this.
This same delta E same E you can also
write in terms of the uh kindinetic
energy which is minus of/
M into V². Do you remember this?
It looks like some of you have forgotten
that. So I hope you know that G mm by R²
is equal to M V² by R. So R R get
cancelled. So half MV²
is equal to G mm by 2R. Now you remember
this.
So honey.
Yes sir.
>> Right. So total energy is minus GMM by
2R total energy of the satellite system.
So delta E once you get that is also
equal to uh negative of E is equal to
negative of/ MV². So delta E in terms of
velocity also you can write which is M
2V delta V.
So in terms of velocity it is minus of
MV delta V. So what if you get delta R
you can relate it to delta V. Equate
these two.
Is it clear?
Clear to all of you.
Everyone type in. See it is
the change is so little that we are
assuming it is going in a server path
and change is so little that in one
revolution delta R is like dr extremely
less. So that is why all of these
approximations are used here to get the
solution
all of you is it clear?
See I have chosen questions which are
not regular types
so that you can see what all things can
happen in gravitation chapter. Okay. So
if you're not getting most of it or
anything
that is good you're learning
something new. You are utilizing your
time properly because every second every
minute you are learning something new.
That is what counts. Okay. Solving
number of questions which you can do in
first attempt is a waste of time.
Now do this.
These are not Olympiads, okay? They are
like proper J advance questions.
But there is a twist in the tail.
So Ry didn't understand what we have to
prove.
>> You have to
basically get a relation between small n
and rest of the thing. That's all.
>> How the variables are connected.
>> No, like that last point. uh
>> remain about the same point on the
equator. What same point?
>> See, same point meaning that it is
uh revolving with the same angular
velocity with the earth. Okay.
Relative to earth, it is I mean it is
revolving with the earth. Is it clear to
everybody?
>> Got it.
>> It's like a geostationary satellite type
of thing.
See again it is a circular motion. So
just find the force towards the center.
And
>> is NR from the surface or from the
center of the earth?
>> Is it not clear? Uh just above the
surface of the earth out to a radius NR.
NR is the radius center.
Whenever something is moving in a circle
just write net force toward the center
is m omega² r.
That's all is there in this question
most probably
got it.
The elevator is not touching the earth.
Okay. It is written that elevator is
just above the surface of the earth. So
there is no question of normal reaction.
Anybody
is getting
Okay, Prano got the answer.
Uh, yes.
Anybody else got the answer?
>> No, sir.
>> Okay.
Fine.
So, this is the Earth.
This is the rod.
It's rotating with omega kn. So even the
rod has to rotate with omega kn and uh
the rod is not touching the earth.
Average density is row posted mega space
out the radius nr.
This is nr.
This is r
h.
So the uh this is the center center of
the rod right. So first we need to find
the force towards the center. Uh so you
know this is like a rigid body
rotating in a circular path. So we just
need to bother
about the what happens to the center of
mass of the rod. Center of mass is
moving in a circle of this radius.
Right?
So this radius
is how much?
This radius is
this is NR.
This distance is NR - R
/ 2. Total length is NR - R. That is NR
- R
/ 2 and add R to it. that is a distance
of the center of mass
distance of the center of mass from the
center of the revolution.
So that is n r + r by 2. This is the
radius.
Then we have to find the net force. So
this is like let's say at a distance of
x this is dx
something similar we did so f
g m
lambda
x dx / x²
and then x goes from
r to
n R - R.
So this is G M lambda.
Those shouldn't go to
they're measuring X from the center of
the fourth ray.
>> Oh, correct. Correct.
Correct.
R to NR right G M by lambda
1x R - 1 by NR
F is equal to G M
the lambda can be written as
lambda
is total mass
divided by length which is nr - r.
This should be equal to m
M is m
omega²
into the radius of revolution.
This equation you just cancel out the
unnecessary terms simplify get the
answer.
We have not done anything great here.
Just found the force
found the radius of revolution and wrote
the centime force is equal to m omega
square r. That's all
clear to all of you any doubts anybody?
Nothing I'm going to next question.
to this
5 to 6 minutes.
Um
both the parts 6 to 7 That's
Do you guys get breaks during the crash
course?
No, sir.
We'll discuss in couple of minutes.
Uh
let's get one hint. How will you find
relate uh maximum distance?
What concept to be used here?
Energy consation.
>> Energy conservation.
How will you identify the point which is
having the maximum distance from the
center? What is that identification?
>> Are we not saying that the entirety of
the kinetic energy gets converted to
potential energy at that particular
point?
>> No, need not be. It will still have some
velocity. The point at which relative
velocity with the center becomes zero.
>> Uh no
but somehat like that
>> the direction of the center rather so
it's not going further away now it's
coming closer.
>> Correct. It is the velocity component
>> uh that that's what I meant component
sorry
>> uh component away from
away along the line joining is zero.
It'll keep on going away away and then
the velocity become perpendicular to the
line joining entire velocity. Right? Now
think over it. Which concept will you
use to relate that point with whatever
point you know initially?
>> So SHM
>> not SHM it comes out of the tunnel right
it goes out. It is moving outside
>> at that specific point. It's in circular
motion at that instant because velocity
is perpendicular to the center.
>> So is it conservation of angular
momentum?
>> Angular momentum. So the these are I
mean you you should be now uh tuning
your
thoughts
uh that whenever you get such scenario
you have to use conservation of angular
momentum because that is where I mean we
used to think that angular momentum is
like not so useful
and not so fundamental
equation. It's just like mathematical
correlation with velocity and
perpendicular distance. But we forget to
use it like how we use conservation of
linear momentum. Start using it whenever
you see that about a point about any
point let us say torque is zero. You can
use the conservation of angular
momentum. For example here once it comes
out
first of all once the particle is inside
there's a normal reaction also due let's
say if it is here there's a normal
reaction which will have torque about
the center. So that is why angular
momentum
is not considered. Oh angular momentum
is written also right. So you need to
get the hint from here itself. Anyways
once it comes out like this then normal
direction becomes zero. Now angular
momentum is conserved because only other
force is gravitational force which is
passing through the center. So about the
center torque is zero. So it goes like
this
and like that right?
No, it will come back. Sorry.
Goes like this and tries to again come
back and fall maybe. Okay.
So maximum distance appears to be
somewhere here.
It is here where the velocity
is making 90° with the line joining. All
right.
So between this point number two and
point number one you can conserve the
angular momentum.
Okay.
Right. But you need to first get this
velocity.
This is v_sub_1.
This is v_sub_2.
How will you get v_sub_1 and v_sub_2?
Right now it is at a distance of rx2
away.
So you need to get uh
only this much part of the earth is
creating the force.
Oh, it will be that formula.
Do you know the potential gravitational
potential inside the solid sphere?
Anybody remembers that expression
inside the solid? G mm by 2 RQ into 3 R²
- small R²
>> by 2 R cube into 3 small R²
>> no capital R² minus small R square
>> this is correct
>> and minus sign like overall
>> this is a minus okay great so basically
first step is to get V_sub1 so between
this point this is point O point 0 and
one we'll use conservation of mechanical
energy why it will not perform SHM so
suppose it is
uh restricted inside the funnel then
it'll perform SHM but suppose at point
number one suppose you use conservation
of mechanical energy okay and you're
getting velocity at point number one to
be zero
then the maximum distance is this
distance only Sorry that distance
distance from the center they're asking
that is r only that is the answer but
suppose you you're getting greater than
zero velocity it means it will come out
so you need to check whether it will be
confined within or not so let's not
assume anything let's find v_sub1 so you
substitute small r equal to rx2 here
uh potential energy is mass into
potential
so that is your u0.
So u0 +/
m v² v not is given
that should be equal to u1 u1 you can
write very easily g mm minus of gmm
minus of gmm by r
+/
m into v1² Now most probably V1 will
come out to be greater than zero.
It is a J advanced question. It can't be
just this much. So V_sub_1 is greater
than zero. Now once you get v_sub_1
then you need to do one more circus here
because this about that point
perpendicular distance is not r
right of this velocity perpendicular
distance from this point line of
velocity is rx2 okay theta and all will
not come so angular momentum of that
v_sub_1 at point number one is m v_sub_1
into rx2
that should be equal to m v2 into this
distance d.
So m and m get cancel. This is your
first equation. Now you have to do
conservation of mechanical energy
between 1 and 2.
So minus of g mm by r +/ m v1² should be
equal to minus of g mm by d +/ m v2². So
solve the 1 and 2 equation to get the
value of d. This is how you do it.
Sir in the first part of the question
they asked if angular momentum is
conserved in the tunnel right so since
at both the middle point and at the end
point the perpendicular distance remains
same from the center
>> so wouldn't the velocity be same if
angular momentum is conserved
>> angular momentum is not conserved as it
is inside the tunnel because there's a
normal reaction also applied that normal
reaction torque is not zero about
Yes sir.
>> Once it is outside of the tunnel then
only the force is passing through the
center of the uh earth. So you can say
that outside of the tunnel angular
momentum is conserved. Inside the tunnel
normalization is there angular momentum
is not conserved. But then yes if it
would have been conserved then velocity
will not change. You're correct to point
out that.
>> So,
>> but the particle inside the tunnel
doesn't necessarily have to touch the
tunnel, right? For the normal reaction
to act.
>> Normal is a contact force. You need a
contact.
>> Okay.
>> And it will touch. It has to touch.
it can't uh I mean when you give the
velocity projectile is fired along a
tunnel from the center that velocity how
will you give suppose you are like okay
no I'll give the velocity if it is
inside the tunnel in the air I'll get so
it becomes a projectile and you'll say
that it will come out uh before it falls
on the ground but tunnel distance is rx2
given so you need to assume that tunnel
is very very uh thin
So you even if you move little bit in
vertical direction you will touch. So
you can't ignore the contact.
>> Okay sir.
>> Uh this is this is like one of those
regular straightforward questions.
this one.
How much is the time? Okay,
you have 6 to 7 minutes. This uh you
know whatever question I'm giving now,
it is pretty much doable. Please attempt
it with full energy. Don't put your
energy down.
done.
>> Yes sir.
>> Hey, is this a regular thing where 20
people join and at the end 13 left?
So this is a good thing I'd say because
normally there are about six people left
by the time the class gets over.
>> Oh,
so this only happened like the last
physics class and this one
>> physics actually J main physics is
easiest of the three subjects but J
advanced physics is toughest of all
three.
So this changes colors very fast.
So
but then the basic theme remains the
same. If you think in a simple manner,
mathematics can be tough. But if your
thought process is simple and
straightforward, you'll be able to
crack.
Don't complicate your thought process
that some random theorem you know or
some expression you remember. J advance
is not about knowing 100 things. It's
about just knowing few things and able
to use them.
Don't run behind new theorems, new
equations and all that. It is all
useless.
Okay. So shall we do it? Anybody about
to get the answer?
Do we have more questions
to simple?
I think that's it. This is after that we
have just straightforward questions.
This is also not tough but I don't know
why you
are not doing it anyways. Shall I do it?
Somebody did. Is it?
No.
Okay. Vital got something.
Okay. Yeah. Yeah. Seems to be correct.
Vital got it.
Got it.
Let's see
anything moving in a circle. What did I
tell you?
Force toward the center is mv² by r or m
omega square r. So let's see that
particle of mass m moves under the
action of central force whose potential
is this.
If this is the potential
uh the field is what
gravitational field do you remember
this?
>> Yes sir.
gravitational field is minus of 3 k r².
Now just like charge into electrical
field is electrical force mass into
gravitational field is gravitational
force.
So uh the force gravitational force is 3
m kr².
I'm ignoring the negative sign just as a
direction.
This should be equal to u m v ² by r
or what energy? Okay.
So m v² is equal to 3 m kr cq. So
kinetic energy is 3x2 mkr cq. This is
kindinetic energy.
What about potential energy?
How do you find potential energy?
Anyone?
>> Mass into potential.
>> Mass into potential. Just like mass into
electrical potential is electrical
potential energy. Mass into
gravitational potential is gravitational
potential energy.
So minus of
m K r cq.
So total energy
is sum of these two. So which is 1 by 2
m k r cq. Now put r equal to a. You'll
get the answer for the total energy.
And the
angular momentum is m vr
right m into v into r. Now how will you
get velocity? So from here from here get
the velocity
in terms of r substitute here you'll get
angular momentum
and then period also you'll get 2 pi r
by v.
again V you can get from here clear to
everyone this is a proper J advanc
question this is how it will be can't be
easier than this
fine
let me see what I what else I have
this question though you might have seen
so many times should not even bother to
equal to half the
did I leave anything
oh above
no
sure or take just for
completeness
we'll do these questions also
solve to get the correct answer
and quickly. Hey,
So I think uh
you all are able to do this after doing
some tricky ones.
Artificial satellite is moving in a
circle orbit around the earth with a
speed equal to half the magnitude of the
escape velocity.
Okay.
Is escape velocity half of it
is this. This is the velocity. Determine
the height.
So, MV² by R height you have to
determine not the radius.
So, R is
GM by V².
So
gm by v² is 1 by 4
2 gm by r
so it is 2 r
2 r you know uh so height is r 2 r minus
r
okay if it is an mcq there will be an
option of 2 r also so if you are in a
hurry you'll mark 2 r and move ahead
There go there go your th00and to 2,000
ranks. Okay. So be very careful in J1s.
It's not about speed. J1s don't hurry up
things.
If a satellite is stopped suddenly in
its orbit and allowed to fall freely
speed at which it hits the surface of
the earth,
it stops. So velocity becomes zero. It
has a potential energy. So, I hope you
can do all of this. I don't need to do
it.
That's it, I guess. Right. So, we'll end
the class here.
And uh
anybody has any doubts in gravitation
from anywhere,
anything you can ask now.
Nothing.
Okay.
>> No sir, no doubts.
>> Take care of your chemistry guys. I have
seen chemistry percentiles of yours are
not great. And remember the rankers
their chemistry is the best.
So
you know learn chemistry. Forget about I
mean it's boring and all that. It's
don't make such excuses. It's not about
boring or something. It's about your
future. It's about your ranks. So
attempt chemistry properly and learn.
There is a time that you can learn you
you can basically uh see what all tricky
things you don't understand of chemistry
and learn them. Okay. Cho. Bye.
>> Thank you sir.
>> Thank you sir. Bye.