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Study of Swept Angle Effects on Grid Fins Aerodynamics Performance

Faza G.A.a, Fadillah H.a, Silitonga F.Y.a, Moelyadi M.A.a

a Department of Aerospace Engineering, Bandung Institute of Technology, Indonesia

Abstract

© Published under licence by IOP Publishing Ltd.Grid fin is an aerodynamic control surface that usually used on missiles and rockets. In the recent several years many researches have conducted to develop a more efficient grid fins. There are many possibilities of geometric combination could be done to improve aerodynamics characteristic of a grid fin. This paper will only discuss about the aerodynamics characteristics of grid fins compared by another grid fins with different swept angle. The methodology that used to compare the aerodynamics is Computational Fluid Dynamics (CFD). The result of this paper might be used for future studies to answer our former question or as a reference for related studies.

Author keywords

Aerodynamic control,Aerodynamics performance,CFD simulations,Grid fin,Lattice Fin,On grids,Swept angle,Swept-Back

Indexed keywords

CFD Simulation,Grid Fin,Lattice Fin,Swept-Back

Funding details

DOI