2012•Unpublished venueRequires access

Solid propellant rocket nozzle design and validation using Finite Difference Method and CFD technique

Gerardo Martín Imbrioscia, Luis Francisco Barceló, Parra Vilar, M. H. Acuña

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Key concepts: Propellant, Nozzle, Computational fluid dynamics, Rocket engine nozzle, Rocket (weapon), Aerospace engineering, Solid-fuel rocket, Engineering

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Solid propellant rocket nozzle design and validation using Finite Difference Method and CFD technique — Research Paper | ScholarLens