Abstrakt

Stability Characteristics of missile due to maneuvering in all six Degree of freedom using CFD simulations

Dr.B.Balakrishna ,G.Sowjanya

This project aims at establishing the stability characteristics of the missile with respect to Angle of attack of the control surfaces, using Computational fluid dynamics Simulations. The drag, lift around the missile will be estimated for various AOA. Based on these simulations, the optimal range of angle of attack in all six Degrees of freedom will be decided