Construction of Airplane Landing Mathematical Models With Drag Chute
(1) Department of Physics, Faculty of Military Mathematics and Natural Sciences, Republic of Indonesia Defense University, Bogor
(2) Department of Physics, Faculty of Military Mathematics and Natural Sciences, Republic of Indonesia Defense University, Bogor
(3) Department of Physics, Faculty of Military Mathematics and Natural Sciences, Republic of Indonesia Defense University, Bogor
(*) Corresponding Author
Abstract
In this article, we analyze the dynamics of a airplane landing using a parachute called a drag chute. As long as the aircraft makes a landing until it comes to a complete stop, the airplane experiences two times the air drag, namely the air resistance that appears before the drag chute is used and after it is used. From the calculation, we obtain that the distance is shorter than without using a drag chute.
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