Optimization of Process Parameters for Flow Nozzle with Different Geometry using Computational Fluid Dynamics Method
Vinayaka Nagarajaiah,
Sara Solomon Raj,
Ayampalayam Nanjappan Swaminathen
et al.
Abstract:A nozzle is a tubular structure designed to facilitate the flow of hot gases. Rocket nozzle designs typically consist of a stationary convergent section and a stationary divergent section. The term "CD" is an abbreviation for "convergent-divergent" and is used to refer to this specific nozzle type. Upgrades are being made to nozzles and other engine components in order to enhance performance and optimise thrust delivery. Application-specific improvements will be made to rocket nozzles and other current combust… Show more
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