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Model Rocket Flow Analysis in ANSYS by juanabel99 is a document available to read on EtoBox.

The document outlines the objectives and problem description for studying turbulent steady 3D flow past the Estes Firestreak SST model rocket at a velocity of 30 m/s. It includes details on simulating the flow in ANSYS Fluent, determining the drag coefficient, and visualizing the flow around the rocket. Additionally, it provides equations and parameters related to drag coefficients and Reynolds numbers for the model rocket components.

Author
juanabel99
Language
EN