Abstract
The advent of the modern cruise missile, with less radar detection and the ability to fly at low altitudes in sub sonic speeds with precise navigation, placed an extensive liability on all weapon systems in defence.The purpose of this project is to present a preliminary analysis and design of a cruise missile which fulfill the mission requirements. This design project comprises the concept exploration and development stages of the full design process. While designing we should take dimensions as per our requirements and should have tolerances to design parts. CATIA V5 is used as design tool. The inlet temperature, pressure, density and altitude are the parameters to analyze the flow properties. The analysis done in the ANSYS WORKBENCH 14.5.This paper discuss the flow of the designed model. In this paper we are going to discuss key aspects in aerodynamics of wing and fin.
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