Convergent Divergent Nozzle Design and Analysis to Increase Working Effectiveness

Abstract

Abstract: Our project's major goal is to develop and examine a Convergent- Divergent rocket nozzle in order to lower nozzle costs. Here, convergent divergent nozzle uses an alternative material. The design is based on earlier designs that served as a guide for our own. A nozzle is a crucial component that merits consideration in this era of expanding rocket propulsion for a variety of uses, including the launch of satellites into space or human missions. With this in mind, a fundamental design is created utilising the understanding of compressible flow, and the resulting thrust is estimated. use the layout established by hand computations. Utilising the ANSYS Fluent programme, the work is done in, the calculations and results are validated.