This analysis report is the first report I wrote as a member of the PARS Rocket Group.
It is a detailed aerodynamic examination of why more fins are not used in standard rockets, rather than three or four.
This report; going beyond the classical rocket designs, which have now become a standard inthe rocketry industry, preferred due to its practicality and various advantages, designed as four equal-sized fins attached to the lower body; the effect of a larger number of additional winglets positioned in different places than the standard fins on the general flow and flight was examined, and the analyzes obtained through Openrocket and Ansys applications were shared on the basis of these examinations.
Some Preview Pictures:
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Halit Yusuf Genç
Engineer For Space 