Difficulty distribution
How the classified questions are distributed by difficulty.
Your cart is empty.
Practice Gravitation - Mechanics - Physics previous year questions organised from real papers, with year-wise coverage and clear topic navigation.
Every graph below is calculated only from this selection.
Year-wise coverage for Gravitation. Each bar uses a separate theme-derived color.
How the classified questions are distributed by difficulty.
MCQ, numerical, multiple-select and other formats found in these papers.
Top subjects by unique question coverage.
Top topics across the included previous year papers.
Top subtopics inside this exact selection.
Question coverage for the most populated papers. Every active PYP paper remains listed below.
Newest papers appear first. Sort by year, question coverage or name.
| Paper | Year / session | Questions in this view | Open |
|---|---|---|---|
| VITEEE 2025 | 2025 | 2 | View paper |
| WB JEE 2024 | 2024 | 1 | View paper |
| WB JEE 2023 | 2023 | 2 | View paper |
| WB JEE 2022 | 2022 | 1 | View paper |
| WB JEE 2021 | 2021 | 1 | View paper |
| WB JEE 2019 | 2019 | 1 | View paper |
| WB JEE 2018 | 2018 | 1 | View paper |
| WB JEE 2008 | 2008 | 2 | View paper |
Practice every matching question in batches of 20, with every available option.
A body of mass m is thrown vertically upward with speed \(\sqrt3\) ve, where ve is the escape velocity of a body from earth surface. The final velocity of the body is
An earth's satellite near the surface of the earth takes about 90 min per revolution. A satellite orbiting the moon also takes about \(90 \mathrm{~min}\) per revolution. Then which of the following is true?
[where \(\rho_{\mathrm{m}}\) is density of the moon and \(\rho_{\mathrm{e}}\) is density of the earth.]
Acceleration due to gravity at a height H from the surface of a planet is the same as that at a depth of H below the surface. If R be the radius of the planet, then H vs. R graph for different planets will be,
A satellite of mass \(\mathrm{m}\) rotates round the earth in a circular orbit of radius R. If the angular momentum of the satellite is J, then its kinetic energy \((\mathrm{K})\) and the total energy (E) of the satellite are
If the Earth is assumed to be a sphere of uniform mass density and its weight on the surface is 200 N , then the weight of the body at a depth halfway to the Earth's center will be
An object is projected from surface of Earth with a kinetic energy twice that of escape energy ' $K$ ', from surface of Earth. It's kinetic energy when it reaches far away from Earth is
The weight of a body on surface of earth is 12.6 N. When it is raised to a height half the radius of earth, its weight will be
If the earth shrinks such that its mass does not change but radius decreases to one quarter of its original value then one complete day will take