Approximation of D.I.Y. Water Rocket Dynamics Including Air Drag

L. Fischer¹ , T. Günther² , L. Herzig³ , T. Jarzina⁴ , F. Klinker⁵ , S. Knipper⁶ , F.G. Schürmann⁷ , M. Wollek⁸

Section:Research Paper, Product Type: Journal-Paper
Vol.6 , Issue.6 , pp.1-13, Dec-2019

CrossRef-DOI:   https://doi.org/10.26438/ijsrmss/v6i6.113

Online published on Dec 31, 2019

Copyright © L. Fischer, T. Günther, L. Herzig, T. Jarzina, F. Klinker, S. Knipper, F.G. Schürmann, M. Wollek . This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
 

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Abstract :
If you want to get accurate predictions for the motion of water and air propelled D.I.Y rockets, neglecting air resistance is not an option. But the theoretical analysis including air drag leads to a system of differential equations which can only be solved numerically. We propose an approximation which simply works by the estimation of a definite integral, and which is even feasible for undergraduate physics courses. The results only slightly deviate from the reference data (received by the Runge-Kutta method). The motion is divided into several flight phases that are discussed separately and the resulting equations are solved by analytic and numeric methods. The different results from the flight phases are collected and are compared to data that has been achieved by well explained and documented experiments. Furthermore, we theoretically estimate the rockets drag coefficient. The result is confirmed by a wind tunnel experiment.

Key-Words / Index Term :
Rocket equation, Thrust, Dynamics, Drag coefficient

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