CFD ANALYSIS FOR MISSILE-FIN CONFIGURATION
Missile is an object or weapon suitable for throwing, projecting or directing at a target. The fin is attached at the end of the missile. Fin is the stabilizing and guiding unit of a missile.
It is an aerodynamic surface of the missile for the purpose of giving directional stability and for good maneuverability. The purpose of this project is to compare maneuverability of missile by using different fin design.
In this study, investigation of aerodynamic coefficient and flow structure in subsonic flow on missile configuration by using different types of fin design. Viscous based model is being used to simulate the flow.
Analysis of fin configuration and its behaviour by changing angle of attack and check which design of fin gives good stability. II
Missile is an object or weapon suitable for throwing, projecting or directing at a target. The fin is attached at the end of the missile. Fin is the stabilizing and guiding unit of a missile.
It is an aerodynamic surface of the missile for the purpose of giving directional stability and for good maneuverability. The purpose of this project is to compare maneuverability of missile by using different fin design.
In this study, investigation of aerodynamic coefficient and flow structure in subsonic flow on missile configuration by using different types of fin design. Viscous based model is being used to simulate the flow.
Analysis of fin configuration and its behaviour by changing angle of attack and check which design of fin gives good stability. II
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