1M. Tech Student, Department of Mechanical Engineering, Gousia College of Engineering, Ramanagara, India
2Assistant Professor, Department of Mechanical Engineering, Gousia College of Engineering, Ramanagara, India
3Principal & Professor, Department of Mechanical Engineering, Gousia College of Engineering, Ramanagara, India
Online published on 21 November, 2017.
In this work an unmanned test rocket structure will be developed for the required dimensions using modelling software using solid works. The each section will be theoretically checked for structural strength after analysing the aerodynamic loads. Later the modelling and meshing will be carried out using ANSYS. The modelled structure will be optimized using Finite element software's and suggestions for the proper geometry will be carried out based on the results.
F E Modelling, aerodynamics load, meshing
