Computational Fluid Dynamics (CFD) Analysis Study On Rocket Nozzles For Design And Performance Optimization - A Review

The nozzle is an important component used extensively in aerospace research and industries. The main component used in rocket engines is the convergent-divergent (CD) nozzle. Researchers all around the world are focused on designing nozzles that meet the current day trends across the aerospace sector. Also, nozzles are an extensive research area in aerospace domains. In engineering and technology, nozzles play an important role. The design and performance optimization of rocket nozzles are crucial nowadays. These optimizations are done with the help of computational fluid dynamics (CFD) analysis. Computational Fluid Dynamics (CFD) is a branch of fluid mechanics that makes use of numerical methods, formulas, and algorithms to solve and analyze fluid flow. Computational fluid dynamics analysis usage in engineering and technology is extensive. Recently, researchers have focussed on the optimization of the design and performance of rocket engine nozzles utilizing computational fluid dynamics techniques. This review paper briefly describes the computational fluid dynamics (CFD) analysis study on various rocket engine nozzles for the design and performance optimization.