Optimal Design and Fabrication of Sharp Throat De Laval Rocket Nozzle Prototype

Abstract

Nowadays the nozzles play a key role in rocket science  and missile technology as we know that nozzles are used to convert 
high pressure energy into kinetic energy in order to produce maximum thrust force. This project deals with the optimal design 
and fabrication of sharp throat De Laval rocket nozzle in order to attain acceralated supersonic velocity from subsonic velocity and 
to obtain maximum thrust force at the divergent section of the nozzle without any flow separation and choking due to shock 
waves at the exit portion of the nozzle.