• C.M.Vamsi Priya

A new nose cones concept that guarantees an addition in act over existing ordinary nose cones is talked about in this paper the term nose cone is utilized to allude to the forward most area of a rocket, guided rocket or air ship. The cone is shaped to offer least aerodynamic resistance. The aerodynamic structure of the nose cone area of any vehicle or body intended to go through a compressible fluid medium, (for example, a rocket or airplane rocket or projectile), a vital issue is the assurance of the nose cone geometrical shape for ideal execution. This undertaking assesses the rocket nose cone analysis by utilizing the accompanying materials, for example, Titanium Grade-I, Ti-6Al-4V and Ti-6Al-6v-2Sn. These are essentially more grounded than industrially unadulterated titanium. A cone display is taken from the concepts of obtuse nose cone and structured in the CAD programming catia. Further this nose cone configuration is imported to the Analysis programming named as Ansys and plays out the Structural analysis. At long last the outcomes are thought about and classified.

NEW AERODYNAMIC DESIGN AND STRUCTURAL ANALYSIS OF MISSILE NOSE CONE USING DIFFERENT MATERIALS

"NEW AERODYNAMIC DESIGN AND STRUCTURAL ANALYSIS OF MISSILE NOSE CONE USING DIFFERENT MATERIALS", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 5, page no.271-276, May-2019, Available :http://www.jetir.org/papers/JETIR1905K37.pdf

"NEW AERODYNAMIC DESIGN AND STRUCTURAL ANALYSIS OF MISSILE NOSE CONE USING DIFFERENT MATERIALS", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 5, page no. pp271-276, May-2019, Available at : http://www.jetir.org/papers/JETIR1905K37.pdf