ANALISIS DOUBLE INTEGRAL PADA MOMEN INERSIA DALAM PESAWAT ATWOOD MENGGUNAKAN KATROL DENGAN PENAMBAHAN MASSA BEBAN

Abstract

In the experiment of the atwood plane there is a perpendicular straight motion (GLB) and a perpendicularly altered geral (GLBB), which is a straight-line motion with a fixed velocity of zero acceleration, so the distance traveled is determined only by a fixed velocity within a certain time . While the GLBB is a straight motion in the horizontal direction with the density that changes at any time due to a fixed acceleration. Not only straight-line motion and straight motion change regularly, but the working principle of the pulley is also applied. The moment of inertia of a pulley is a measure of the inertia of a pulley to rotate or change its rotational state when there is a resultant moment of force acting on it. The moment of inertia of this pulley can be determined first by using a conceptual and mathematical approach through translation by using differential and integral techniques, and the second is by empirical approach through experiment, the moment of inertia of a pulley will be determined by using empirical approach through experiment and mathematical physics calculation. The double integral used in this study is a double integral, where the application in physics is a moment of inertia. Atwood aircraft is an experimental tool that is often used to observe the laws of mechanics on the motion of accelerated regularly