JEE Main 2021 (Online) 24th February Morning Slot | Rotational Motion Question 66 | Physics

JEE Main 2021 (Online) 24th February Morning Slot

MCQ (Single Correct Answer)

-1

Moment of inertia (M. I.) of four bodies, having same mass and radius, are reported as;

I₁ = M.I. of thin circular ring about its diameter,

I₂ = M.I. of circular disc about an axis perpendicular to disc and going through the centre,

I₃ = M.I. of solid cylinder about its axis and

I₄ = M.I. of solid sphere about its diameter.

Then :

I₁ = I₂ = I₃ > I₄

I₁ + I₃ < I₂ + I₄

I₁ = I₂ = I₃ < I₄

I₁ + I₂ = I₃ + $${5 \over 2}$$ I₄

JEE Main 2020 (Online) 6th September Evening Slot

MCQ (Single Correct Answer)

-1

The linear mass density of a thin rod AB of length L varies from A to B as
$$\lambda \left( x \right) = {\lambda _0}\left( {1 + {x \over L}} \right)$$, where x is the distance from A. If M is the mass of the rod then its moment of inertia about an axis passing through A and perpendicular to the rod is :

$${2 \over 5}M{L^2}$$

$${5 \over {12}}M{L^2}$$

$${7 \over {18}}M{L^2}$$

$${3 \over 7}M{L^2}$$

JEE Main 2020 (Online) 6th September Morning Slot

MCQ (Single Correct Answer)

-1

Four point masses, each of mass m, are fixed at the corners of a square of side $$l$$. The square is rotating with angular frequency $$\omega $$, about an axis passing through one of the corners of the square and parallel to its diagonal, as shown in the figure. The angular momentum of the square about this axis is : JEE Main 2020 (Online) 6th September Morning Slot Physics - Rotational Motion Question 72 English

JEE Main 2020 (Online) 6th September Morning Slot Physics - Rotational Motion Question 72 English

3m$$l$$²$$\omega $$

4m$$l$$²$$\omega $$

m$$l$$²$$\omega $$

2m$$l$$²$$\omega $$

JEE Main 2020 (Online) 6th September Morning Slot

MCQ (Single Correct Answer)

-1

A satellite is in an elliptical orbit around a planet P. It is observed that the velocity of the satellite when it is farthest from the planet is 6 times less than that when it is closest to the planet. The ratio of distances between the satellite and the planet at closest and farthest points is:

1 : 2

1 : 3

1 : 6

3 : 4

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